U.S. patent application number 10/719073 was filed with the patent office on 2008-11-20 for apparatus for performing heat-exchanging chemical reactions.
This patent application is currently assigned to Cepheid. Invention is credited to Ronald Chang, Lee A. Christel, Douglas B. Dority, Kurt E. Petersen, Robert Yuan.
Application Number | 20080286151 10/719073 |
Document ID | / |
Family ID | 23860833 |
Filed Date | 2008-11-20 |
United States Patent
Application |
20080286151 |
Kind Code |
A1 |
Chang; Ronald ; et
al. |
November 20, 2008 |
APPARATUS FOR PERFORMING HEAT-EXCHANGING CHEMICAL REACTIONS
Abstract
An apparatus for controlling the temperature of a reaction
mixture contained in a chamber of a reaction vessel comprises a
thermal surface for contacting a flexible wall of the chamber and
an automated machine for increasing the pressure in the chamber.
The pressure increase in the chamber is sufficient to force the
flexible wall to conform to the thermal surface for good thermal
conductance. The apparatus also includes at least one thermal
element for heating or cooling the surface to induce a temperature
change within the chamber.
Inventors: |
Chang; Ronald; (Redwood
City, CA) ; Dority; Douglas B.; (Mill Valley, CA)
; Christel; Lee A.; (Palo Alto, CA) ; Yuan;
Robert; (Belmont, CA) ; Petersen; Kurt E.;
(San Jose, CA) |
Correspondence
Address: |
TOWNSEND AND TOWNSEND AND CREW, LLP
TWO EMBARCADERO CENTER, EIGHTH FLOOR
SAN FRANCISCO
CA
94111-3834
US
|
Assignee: |
Cepheid
Sunnyvale
CA
|
Family ID: |
23860833 |
Appl. No.: |
10/719073 |
Filed: |
November 21, 2003 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
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09468690 |
Dec 21, 1999 |
6660228 |
|
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10719073 |
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Current U.S.
Class: |
422/68.1 |
Current CPC
Class: |
B01J 2219/00963
20130101; B01L 2300/1827 20130101; F28D 2021/0077 20130101; B01L
2300/0858 20130101; B01J 2219/0097 20130101; B01J 2219/00873
20130101; F28F 13/00 20130101; B01L 9/00 20130101; B01L 3/508
20130101; B01L 2300/042 20130101; B01J 19/0093 20130101; G01N
2035/0405 20130101; B01J 2219/00788 20130101; G01N 21/0332
20130101; B01L 7/52 20130101; Y10T 436/2575 20150115; G01N 35/0099
20130101; G01N 2035/00376 20130101 |
Class at
Publication: |
422/68.1 |
International
Class: |
G01N 33/48 20060101
G01N033/48 |
Goverment Interests
[0002] This invention was made with Government support under
contract DAAM01-96-C-0061 awarded by the U.S. Army. The Government
has certain rights in the invention.
Claims
1. An apparatus for controlling the temperature of a reaction
mixture, the apparatus comprising: a) a reaction vessel having a
chamber for holding the mixture, the vessel comprising: i) a rigid
frame defining side walls of the chamber, wherein the frame further
includes a port and a channel connecting the port to the chamber;
and ii) at least one flexible sheet attached to the rigid frame to
form a major wall of the chamber; b) at least one thermal surface
for contacting the major wall; c) an automated machine, comprising
a pick-and-place machine for inserting a plunger into the channel
to compress gas in the vessel, thereby increasing the pressure in
the chamber, wherein the pressure increase in the chamber is
sufficient to force the major wall to conform to the thermal
surface; and d) at least one thermal element for heating or cooling
the surface to induce a temperature change within the chamber.
2. The apparatus of claim 1, wherein the vessel includes first and
second flexible sheets attached to opposite sides of the rigid
frame to form opposing major walls of the chamber, the apparatus
includes first and second thermal surfaces formed by opposing
plates positioned to receive the chamber between them, and the
pressure increase in the chamber is sufficient to force the major
walls to contact and conform to the inner surfaces of the
plates.
3. The apparatus of claim 2, wherein each of the plates comprises a
ceramic material, and wherein each of the plates has a thickness
less than or equal to 1 mm.
4. The apparatus of claim 2, wherein each of the plates has a
resistive heating element coupled thereto.
5. The apparatus of claim 4, wherein the heating element comprises
a film.
6. The apparatus of claim 2, wherein each of the plates has a
thermal mass less than 5 J/.degree. C.
7. The apparatus of claim 2, wherein each of the plates has a
thermal mass less than 3 J/.degree. C.
8. The apparatus of claim 2, wherein each of the plates has a
thermal mass less than 1 J/.degree. C.
9. The apparatus of claim 2, further comprising a support structure
for holding the plates in an opposing relationship to each other,
the support structure comprising: a) a mounting plate having a slot
therein; b) spacing posts extending from the mounting plate on
opposite sides of the slot, wherein each of the spacing posts has
indentations formed on opposite sides thereof for receiving the
edges of the plates; and c) retention clips for holding the edges
of the plates in the indentations.
10. (canceled)
11. The apparatus of claim 1, wherein the frame includes an inner
surface defining the channel, and wherein the inner surface has at
least one pressure control groove formed therein, the pressure
control groove extending to a predetermined depth in the channel to
allow gas to escape from the vessel until the plunger reaches the
predetermined depth.
12. The apparatus of claim 1, wherein the plunger has a pressure
stroke sufficient to increase the pressure in the chamber to at
least 2 psi above the ambient pressure external to the vessel.
13. The apparatus of claim 1, wherein the automated machine
comprises: a) a machine head having an axial bore for communicating
with the channel of the vessel; and b) a pressure source for
pressurizing the chamber through the bore in the machine head.
14. The apparatus of claim 13, further comprising an adapter for
placing the bore in fluid communication with the channel, wherein
the adapter is sized to be inserted into the channel such that the
adapter establishes a seal with the walls of the channel.
15. The apparatus of claim 14, wherein the adapter includes a valve
for preventing fluid from escaping from the vessel.
16. The apparatus of claim 1, further comprising an elastomeric
plug inserted into the channel, wherein the automated machine
comprises: a) means for inserting a needle through the plug; and b)
a pressure source for injecting fluid into the vessel through the
needle.
17. The apparatus of claim 16, wherein the needle includes a first
bore for dispensing the fluid into the vessel and a second bore for
venting gas from the vessel, and wherein the first bore has a
length greater than the second bore.
18. The apparatus of claim 1, wherein the automated machine
comprises a platen for heat sealing a film or foil to the vessel to
seal the port and reduce the volume of the channel.
19. The apparatus of claim 1, wherein: a) at least two of the side
walls of the chamber are optically transmissive and angularly
offset from each other; b) the apparatus further comprises an
optics system having at least one light source for exciting the
mixture through a first one of the optically transmissive side
walls and having at least one detector for detecting light emitted
from the chamber through a second one of the optically transmissive
side walls.
20. The apparatus of claim 19, wherein: a) the apparatus includes
first and second thermal surfaces formed by opposing plates
positioned to receive the chamber of the vessel between them; and
b) each of the plates has first and second edges angularly offset
from each other by substantially the same angle that the optically
transmissive side walls are offset from each other, and the plates
are positioned to receive the chamber between them such that the
first optically transmissive side wall is positioned substantially
adjacent and parallel to the first bottom edge of each plate and
such that the second optically transmissive side wall is positioned
substantially adjacent and parallel to the second bottom edge of
each plate.
21. The apparatus of claim 19, wherein the optically transmissive
side walls are angularly offset from each other by about
90.degree..
22. The apparatus of claim 19, wherein at least two additional side
walls of the chamber have retro-reflective faces.
23. The apparatus of claim 19, wherein the ratio of the width the
chamber to the thickness of the chamber is at least 4:1, and
wherein the chamber has a thickness in the range of 0.5 to 2
mm.
24. The apparatus of claim 19, wherein the plates, thermal element,
and optics system are incorporated into a heat-exchanging module,
the apparatus further comprises a base instrument for receiving the
heat-exchanging module, and the base instrument includes processing
electronics for controlling the operation of the module.
25. The apparatus of claim 24, wherein the heat-exchanging module
further comprises a housing and a cooling element disposed within
the housing for cooling the reaction mixture contained in the
chamber.
26. The apparatus of claim 24, wherein the base instrument is
constructed to receive and control a plurality of such
heat-exchanging modules.
27. The apparatus of claim 26, further comprising at least one
computer for controlling the base instrument.
28. An apparatus for controlling the temperature of a reaction
mixture the apparatus comprising: a) a reaction vessel having a
reaction chamber and at least one port for adding fluid to the
chamber, and wherein the chamber has at least one flexible wall; b)
a thermal surface for contacting the flexible wall; c) an automated
machine for increasing the pressure in the chamber, comprising i) a
machine head having a bore for communicating with the vessel; and
ii) a pressure source for pressuring the chamber through the
machine head, wherein the pressure increase in the chamber is
sufficient to force the flexible wall to contact and conform to the
thermal surface; and d) at least one thermal element for heating or
cooling the thermal surface to induce a temperature change within
the chamber.
29. The apparatus of claim 28, wherein the vessel further comprises
a first and a second major flexible wall, and wherein the apparatus
includes first and second thermal surfaces formed by opposing
plates positioned to receive the chamber of the vessel between
them, and wherein each of the plates has a heating element coupled
thereto.
30. The apparatus of claim 29, wherein each of the plates has a
thermal mass less than 5 J/.degree. C.
31. The apparatus of claim 29, wherein each of the plates has a
thermal mass less than 1 J/.degree. C.
32. The apparatus of claim 28, wherein the vessel includes a
channel connecting the port to the chamber, and wherein the
automated machine comprises a pick-and-place machine for inserting
a plunger into the channel to compress gas in the vessel.
33. (canceled)
34. The apparatus of claim 28, further comprising an adapter for
placing the machine head in fluid communication with the vessel,
wherein the vessel includes a channel connecting the port to the
chamber, and wherein the adapter is sized to be inserted into the
channel such that the adapter establishes a seal with the walls of
the channel.
35. The apparatus of claim 28, further comprising an adapter for
placing the machine head in fluid communication with the vessel,
wherein the adapter includes a valve for preventing fluid from
escaping from the vessel.
36. The apparatus of claim 28, wherein the automated machine
further comprises means for dispensing fluid into the vessel
through the machine head.
37. The apparatus of claim 28, wherein the vessel further
comprises: a) a channel connecting the port to the chamber; b) an
elastomeric plug inserted into the channel; and wherein the
automated machine further comprises: a) a needle for inserting
through the plug; b) means for inserting the needle through the
plug; and c) means for injecting fluid into the vessel through the
needle.
38. The apparatus of claim 37, wherein the needle includes a first
bore for dispensing the fluid into the vessel and a second bore for
venting gas from the vessel, and wherein the first bore has a
length greater than the second bore.
39. The apparatus of claim 28, wherein the automated machine
comprises a platen for heat sealing a film or foil to the vessel to
seal the port.
40. The apparatus of claim 28, further comprising an optics system
for optically interrogating the mixture contained in the chamber
through first and second optically transmissive walls of the
vessel, the optics system having at least one light source for
exciting the mixture through the first wall and having at least one
detector for detecting light emitted from the chamber through the
second wall.
41. The apparatus of claim 40, wherein the plates, heating
elements, and optics system are incorporated into a heat-exchanging
module, the apparatus further comprises a base instrument for
receiving the heat-exchanging module, and the base instrument
includes processing electronics for controlling the operation of
the module.
42. The apparatus of claim 29, wherein each of the plates comprises
a ceramic material, and wherein each of the plates has a thickness
less than or equal to 1 mm.
43. The apparatus of claim 29, wherein the heating element
comprises a film.
44. The apparatus of claim 29, further comprising a support
structure for holding the plates in an opposing relationship to
each other, the support structure comprising: a) a mounting plate
having a slot therein; b) spacing posts extending from the mounting
plate on opposite sides of the slot, wherein each of the spacing
posts has indentations formed on opposite sides thereof for
receiving the edges of the plates; and c) retention clips for
holding the edges of the plates in the indentations.
45. The apparatus of claim 32, wherein an inner surface of the
channel has at least one pressure control groove formed therein,
the pressure control groove extending to a predetermined depth in
the channel to allow gas to escape from the vessel until the
plunger reaches the predetermined depth.
46. The apparatus of claim 45, wherein the plunger has a pressure
stroke sufficient to increase the pressure in the chamber to at
least 2 psi above the ambient pressure external to the vessel.
47. The apparatus of claim 28, wherein a rigid frame defines side
walls of the chamber, and wherein: a) at least two of the side
walls of the chamber are optically transmissive and angularly
offset from each other; b) the apparatus further comprises an
optics system having at least one light source for exciting the
mixture through a first one of the optically transmissive side
walls and having at least one detector for detecting light emitted
from the chamber through a second one of the optically transmissive
side walls.
48. The apparatus of claim 47, wherein: a) the apparatus includes
first and second thermal surfaces formed by opposing plates
positioned to receive the chamber of the vessel between them; and
b) each of the plates has first and second edges angularly offset
from each other by substantially the same angle that the optically
transmissive side walls are offset from each other, and the plates
are positioned to receive the chamber between them such that the
first optically transmissive side wall is positioned substantially
adjacent and parallel to the first bottom edge of each plate and
such that the second optically transmissive side wall is positioned
substantially adjacent and parallel to the second bottom edge of
each plate.
49. The apparatus of claim 47, wherein the optically transmissive
side walls are angularly offset from each other by about
90.degree..
50. The apparatus of claim 47, wherein at least two additional side
walls of the chamber have retro-reflective faces.
51. The apparatus of claim 47, wherein the ratio of the width of
the chamber to the thickness of the chamber is at least 4:1, and
wherein the chamber has a thickness in the range of 0.5 to 2.0
mm.
52. The apparatus of claim 41, wherein the heat-exchanging module
further comprises a housing and a cooling element disposed within
the housing for cooling the reaction mixture contained in the
chamber.
53. The apparatus of claim 41, wherein the base instrument is
constructed to receive and control a plurality of such
heat-exchanging modules.
54. The apparatus of claim 53, further comprising at least one
computer for controlling the base instrument.
Description
RELATED APPLICATION INFORMATION
[0001] This application is a continuation in part of U.S.
application Ser. No. 09/194,374 filed Nov. 24, 1998. This
application is also related to U.S. application Ser. No. 09/275,061
filed Mar. 23, 1999 and Ser. No. 09/314,605 filed May 19, 1999. All
of these applications are incorporated by reference herein for all
purposes.
FIELD OF THE INVENTION
[0003] The present invention relates to an apparatus for performing
heat-exchanging, chemical reactions and for optically detecting a
reaction product.
BACKGROUND OF THE INVENTION
[0004] There are many applications in the field of chemical
processing in which it is desirable to precisely control the
temperature of reaction mixtures (e.g., biological samples mixed
with chemicals or reagents), to induce rapid temperature changes in
the mixtures, and to detect target analytes in the mixtures.
Applications for such heat-exchanging chemical reactions may
encompass organic, inorganic, biochemical and molecular reactions,
and the like. Examples of thermal chemical reactions include
isothermal nucleic acid amplification, thermal cycling nucleic acid
amplification, such as the polymerase chain reaction (PCR), ligase
chain reaction (LCR), self-sustained sequence replication, enzyme
kinetic studies, homogeneous ligand binding assays, and more
complex biochemical mechanistic studies that require complex
temperature changes. Temperature control systems also enable the
study of certain physiologic processes where a constant and
accurate temperature is required.
[0005] One of the most popular uses of temperature control systems
is for the performance of PCR to amplify a segment of nucleic acid.
In this well known methodology, a DNA template is used with a
thermostable DNA polymerase, nucleoside triphosphates, and two
oligonucleotides with different sequences, complementary to
sequences that lie on opposite strands of the template DNA and
which flank the segment of DNA that is to be amplified ("primers").
The reaction components are cycled between a first temperature
(e.g., 95.degree. C.) for denaturing double stranded template DNA,
followed by a second temperature (e.g., 40-60.degree. C.) for
annealing of primers, and a third temperature (e.g., 70-75.degree.
C.) for polymerization. For some newer assays, the annealing and
polymerization may be performed at the same temperature (e.g.
55-60.degree. C.), so that only two set point temperatures are
required in each thermal cycle. Repeated cycling provides
exponential amplification of the template DNA.
[0006] Nucleic acid amplification may be applied to the diagnosis
of genetic disorders; the detection of nucleic acid sequences of
pathogenic organisms in a variety of samples including blood,
tissue, environmental, air borne, and the like; the genetic
identification of a variety of samples including forensic,
agricultural, veterinarian, and the like; the analysis of mutations
in activated oncogenes, detection of contaminants in samples such
as food; and in many other aspects of molecular biology.
Polynucleotide amplification assays can be used in a wide range of
applications such as the generation of specific sequences of cloned
double-stranded DNA for use as probes, the generation of probes
specific for uncloned genes by selective amplification of
particular segments of cDNA, the generation of libraries of cDNA
from small amounts of mRNA, the generation of large amounts of DNA
for sequencing and the analysis of mutations.
[0007] A preferred detection technique for chemical or biochemical
analysis is optical interrogation, typically using fluorescence or
chemiluminescence measurements. For ligand-binding assays,
time-resolved fluorescence, fluorescence polarization, or optical
absorption is often used. For PCR assays, fluorescence chemistries
are often employed.
[0008] Conventional instruments for conducting thermal reactions
and for optically detecting the reaction products typically
incorporate a block of metal having as many as ninety-six conical
reaction tubes. The metal block is heated and cooled either by a
Peltier heating/cooling apparatus or by a closed-loop liquid
heating/cooling system in which liquid flows through channels
machined into the block. Such instruments incorporating a metal
block are described in U.S. Pat. No. 5,038,852 to Johnson and U.S.
Pat. No. 5,333,675 to Mullis.
[0009] These conventional instruments have several disadvantages.
First, due to the large thermal mass of a metal block, the heating
and cooling rates in these instruments are limited to about
1.degree. C./sec resulting in longer processing times. For example,
in a typical PCR application, fifty cycles may require two or more
hours to complete. With these relatively slow heating and cooling
rates, some processes requiring precise temperature control are
inefficient. For example, reactions may occur at the intermediate
temperatures, creating unwanted and interfering side products, such
as PCR "primer-dimers" or anomalous amplicons, which are
detrimental to the analytical process. Poor control of temperature
also results in over-consumption of expensive reagents necessary
for the intended reaction.
[0010] A second disadvantage of these conventional instruments is
that they typically do not permit real-time optical detection or
continuous optical monitoring of the chemical reaction. For
example, in conventional thermal cycling instruments, optical
fluorescence detection is typically accomplished by guiding an
optical fiber to each of ninety-six reaction sites in a metal
block. A central high power laser sequentially excites each
reaction site and captures the fluorescence signal through the
optical fiber. Since all of the reaction sites are sequentially
excited by a single laser and since the fluorescence is detected by
a single spectrometer and photomultiplier tube, simultaneous
monitoring of each reaction site is not possible.
[0011] Some of the instrumentation for newer processes requiring
faster thermal cycling times has recently become available. One
such device is disclosed by Northrup et al. in U.S. Pat. No.
5,589,136. The device includes a silicon-based, sleeve-type
reaction chamber that combines heaters, such as doped polysilicon
for heating, and bulk silicon for convection cooling. The device
optionally includes a secondary tube (e.g., plastic) for holding
the sample. In operation, the tube containing the sample is
inserted into the silicon sleeve. Each sleeve also has its own
associated optical excitation source and fluorescence detector for
obtaining real-time optical data. This device permits faster
heating and cooling rates than the instruments incorporating a
metal block described above. There are, however, several
disadvantages to this device in its use of a micromachined silicon
sleeve. A first disadvantage is that the brittle silicon sleeve may
crack and chip. A second disadvantage is that it is difficult to
micromachine the silicon sleeve with sufficient accuracy and
precision to allow the sleeve to precisely accept a plastic tube
that holds the sample. Consequently, the plastic tube may not
establish optimal thermal contact with the silicon sleeve.
[0012] Another instrument is described by Wittwer et al. in "The
LightCycler.TM.: A Microvolume Multisample Fluorimeter with Rapid
Temperature Control", BioTechniques, Vol. 22, pgs. 176-181, January
1997. The instrument includes a circular carousel for holding up to
thirty-two samples. The temperature of the samples is controlled by
a central heating cartridge and a fan positioned in a central
chamber of the carousel. In operation, the samples are placed in
capillaries which are held by the carousel, and a stepper motor
rotates the carousel to sequentially position each of the samples
over an optics assembly. Each sample is optically interrogated
through a capillary tip by epi-illumination. This instrument also
permits faster heating and cooling rates than the metal blocks
described above. Unfortunately, this instrument is not easily
configured for commercial, high throughput diagnostic
applications.
SUMMARY
[0013] The present invention overcomes the disadvantages of the
prior art by providing an improved apparatus for thermally
controlling and optically interrogating a reaction mixture. In
contrast to the prior art instruments described above, the
apparatus of the present invention permits extremely rapid heating
and cooling of the mixture, ensures optimal thermal transfer
between the mixture and heating or cooling elements, provides
real-time optical detection and monitoring of reaction products
with increased detection sensitivity, and is easily configured for
automated, high throughput applications. The apparatus is useful
for performing heat-exchanging chemical reactions, such as nucleic
acid amplification.
[0014] In a preferred embodiment, the apparatus includes a reaction
vessel having a chamber for holding the mixture. The vessel has a
rigid frame defining the side walls of the chamber, and at least
one flexible sheet attached to the rigid frame to form a major wall
of the chamber. The rigid frame further includes a port and a
channel connecting the port to the chamber to permit easy filling,
sealing, and pressurization of the chamber. The apparatus also
includes at least one thermal surface for contacting the flexible
major wall of the chamber. The apparatus further includes a device
for increasing the pressure in the chamber. The pressure increase
in the chamber is sufficient to force the flexible major wall to
contact and conform to the thermal surface, thus ensuring optimal
thermal conductance between the thermal surface and the chamber.
The apparatus also includes one or more thermal elements (e.g., a
heating element, thermoelectric device, heat sink, fan, or peltier
device) for heating or cooling the thermal surface to induce a
temperature change within the chamber.
[0015] In the preferred embodiment, the reaction vessel includes
first and second flexible sheets attached to opposite sides of the
rigid frame to form opposing major walls of the chamber. In this
embodiment, the apparatus includes first and second thermal
surfaces formed by first and second opposing plates positioned to
receive the chamber of the vessel between. When the pressure in the
chamber is increased, the flexible major walls expand outwardly to
contact and conform to the inner surfaces of the plates. A
resistive heating element, such as a thick or thin film resistor,
is coupled to each plate for heating the plates. In addition, the
apparatus includes a cooling device, such as a fan, for cooling the
plates. Each of the plates is preferably constructed of a ceramic
material and has a thickness less than or equal to 1 mm for low
thermal mass. In particular, it is presently preferred that each of
the plates have a thermal mass less than about 5 J/.degree. C.,
more preferably less than 3 J/.degree. C., and most preferably less
than 1 J/.degree. C. to enable extremely rapid heating and cooling
rates.
[0016] The apparatus also preferably includes a support structure
for holding the plates in an opposing relationship to each other.
In the preferred embodiment, the support structure comprises a
mounting plate having a slot therein, and spacing posts extending
from the mounting plate on opposite sides of the slot. Each of the
spacing posts has indentations formed on opposite sides thereof for
receiving the edges of the plates. Retention clips hold the edges
of the plates in the indentations formed in the spacing posts. The
slot in the mounting plate enables insertion of the vessel between
the plates.
[0017] The pressurization of the chamber ensures that the flexible
major walls of the vessel are forced to contact and conform to the
inner surfaces of the plates, thus guaranteeing optimal thermal
contact between the major walls and the plates. In the preferred
embodiment, the device for increasing pressure in the chamber
comprises a plunger which is inserted into the channel to compress
gas in the vessel and thereby increase pressure in the chamber. The
plunger preferably has a pressure stroke in the channel sufficient
to increase pressure in the chamber to at least 2 psi of above the
ambient pressure external to the vessel, and more preferably to a
pressure in the range of 8 to 15 psi above the ambient pressure. In
the preferred embodiment, the length of the pressure stroke is
controlled by one or more pressure control grooves formed in the
inner surface of the frame that defines the channel. The pressure
control grooves extend from the port to a predetermined depth in
the channel to allow gas to escape from the channel and thereby
prevent pressurization of the chamber until the plunger reaches the
predetermined depth. When the plunger reaches the predetermined
depth, it establishes a seal with the walls of the channel and
begins the pressure stroke. The pressure control grooves provide
for highly controllable pressurization of the chamber and help
prevent misalignment of the plunger in the channel.
[0018] The reaction vessel may be filled and pressurized manually
by a human operator, or alternatively, the apparatus may include an
automated machine for filling and pressurizing the vessel. In the
automated embodiment, the apparatus preferably includes a
pick-and-place machine having a pipette for filling the vessel and
having a machine tip for inserting the plunger into the channel
after filling. The plunger preferably includes a cap having a
tapered engagement aperture for receiving and establishing a fit
with the machine tip, thereby enabling the machine tip to pick and
place the plunger into the channel.
[0019] In a second embodiment of the invention, the pressurization
of vessel is performed by a pick-and-place machine having a machine
head for addressing the vessel. The machine head has an axial bore
for communicating with the channel. The pick-and-place machine also
includes a pressure source in fluid communication with the bore for
pressurizing the chamber of the vessel through the bore. In this
embodiment, the apparatus also preferably includes a disposable
adapter for placing the bore in fluid communication with the
channel. The adapter is sized to be inserted into the channel such
that the adapter establishes a seal with the walls of the channel.
The disposable adapter preferably includes a valve (e.g., a check
valve) for preventing fluid from escaping from the vessel.
[0020] In a third embodiment of the invention, the device for
increasing pressure in the chamber comprises an elastomeric plug
which is inserted into the channel, and a needle inserted through
the plug for injecting fluid into the vessel. The needle may be
used to inject the reaction mixture into the chamber, followed by
air or another suitable gas to increase pressure in the chamber.
The reaction vessel may be filled and pressurized in this manner by
a human operator, or alternatively, the apparatus may include an
automated machine for filling and pressurizing the chamber. In the
automated embodiment, the apparatus includes a machine for
inserting the needle through the plug, and the machine includes a
pressure source for injecting fluid into the vessel through the
needle.
[0021] In a fourth embodiment of the invention, the device for
pressurizing the chamber comprises a platen for heat sealing a film
or foil to the vessel. The foil is preferably sealed to the portion
of the frame defining the port. Heat sealing the film or foil to
the vessel seals the port and collapses an end of the channel to
reduce the volume of the vessel and thereby increase pressure in
the chamber. The reaction vessel may be heat sealed in this manner
by a human operator, or alternatively, the apparatus may include an
automated machine, e.g. a press, for sealing the vessel.
[0022] The apparatus of the present invention permits real-time
monitoring and detection of reaction products in the vessel with
improved optical sensitivity. In the preferred embodiment, at least
two of the side walls of the chamber are optically transmissive and
angularly offset from each other, preferably by an angle of about
90.degree.. The apparatus further comprises an optics system for
optically interrogating the mixture contained in the chamber
through the optically transmissive side walls. The optics system
includes at least one light source for exciting the mixture through
a first one of the side walls, and at least one detector for
detecting light emitted from the chamber through a second one of
the side walls.
[0023] Optimum optical sensitivity may be attained by maximizing
the optical sampling path length of both the light beams exciting
the labeled analytes in the reaction mixture and the emitted light
that is detected. The thin, wide reaction vessel of the present
invention optimizes detection sensitivity by providing maximum
optical path length per unit analyte volume. In particular, the
vessel is preferably constructed such that the ratio of the width
of the chamber to the thickness of the chamber is at least 4:1, and
such that the chamber has a thickness in the range of 0.5 to 2 mm.
These parameters are presently preferred to provide a vessel having
a relatively large average optical path length through the chamber,
while still keeping the chamber sufficiently thin to allow for
extremely rapid heating and cooling of the reaction mixture.
[0024] The apparatus of the present invention may be configured as
a small hand-held instrument, or alternatively, as a large
instrument with multiple reaction sites for simultaneously
processing hundreds of samples. In high throughput embodiments, the
plates, heating and cooling elements, and optics are preferably
disposed in a single housing to form an independently controllable,
heat-exchanging module with detection capability. The apparatus
includes a base instrument for receiving a plurality of such
modules, and the base instrument includes processing electronics
for independently controlling the operation of each module. Each
module provides a reaction site for thermally processing a sample
contained in a reaction vessel and for detecting one or more target
analytes in the sample. The apparatus may also include a computer
for controlling the base instrument.
BRIEF DESCRIPTION OF THE DRAWINGS
[0025] FIG. 1 is a partially exploded, isometric view of a reaction
vessel according to a first embodiment of the present invention in
which the major walls of the reaction chamber are removed to show
the interior of the chamber.
[0026] FIG. 2 is a front view of the vessel of FIG. 1.
[0027] FIG. 3 is a top view of a plunger cap of the vessel of FIG.
1.
[0028] FIG. 4 is another front view of the vessel of FIG. 1.
[0029] FIG. 5 is a side view of the vessel of FIG. 1 inserted into
a thermal sleeve formed by opposing plates.
[0030] FIG. 6 is a front view of one of the plates of FIG. 5.
[0031] FIGS. 7A-7D are schematic, cross-sectional views of a
plunger being inserted into a channel of the reaction vessel of
FIG. 1.
[0032] FIG. 8 is a schematic, front view of a heat-exchanging
module according to the present invention having a thermal sleeve,
a pair of optics assemblies, and a cooling system. The reaction
vessel of FIG. 1 is inserted into the thermal sleeve.
[0033] FIG. 9 is an exploded view of a support structure for
holding the plates of FIG. 5.
[0034] FIGS. 10-11 are assembled views of the support structure of
FIG. 9.
[0035] FIG. 12 is an isometric view of the reaction vessel of FIG.
1 inserted between the plates of FIG. 5.
[0036] FIG. 13 is an isometric view showing the exterior of one the
optics assemblies of FIG. 8.
[0037] FIG. 14 is an isometric view of the optics assembly of FIG.
13, the plates of FIG. 5 in contact with the optics assembly, and
the vessel of FIG. 1 positioned above the plates.
[0038] FIGS. 15A and 15B are graphs showing the excitation and
emission spectra, respectively, of four dyes often used in thermal
reactions.
[0039] FIG. 15C shows the effects of filtering the outputs of green
and blue LEDs to provide distinct excitation wavelength ranges.
[0040] FIG. 15D shows the effects of filtering light emitted from
each of the four dyes of FIGS. 15A-B to form distinct emission
wavelength ranges.
[0041] FIG. 16 is a plan view of an optical excitation assembly of
the module of FIG. 8.
[0042] FIG. 17 is an exploded view of the excitation assembly of
FIG. 16.
[0043] FIG. 18 is a plan view of an optical detection assembly of
the module of FIG. 8.
[0044] FIG. 19 is an exploded view of the detection assembly of
FIG. 18.
[0045] FIG. 20 is an isometric view of a multi-site reactor system
according to the present invention.
[0046] FIG. 21 is a schematic, block diagram of another multi-site
reactor system having multiple thermal cycling instruments
daisy-chained to a computer and a power source.
[0047] FIG. 22 is a schematic, block diagram of a base instrument
of the system of FIG. 20.
[0048] FIG. 23 is a schematic, block diagram of the electronic
components of the module of FIG. 8.
[0049] FIG. 24 is a schematic diagram of a pick-and-place machine
having a pipette for filling the reaction vessel of FIG. 1.
[0050] FIG. 25 is a schematic diagram of the pick-and-place machine
of FIG. 24 inserting a plunger into the vessel of FIG. 1.
[0051] FIG. 26 is a schematic, front view of a reaction vessel
according to another embodiment of the invention.
[0052] FIG. 27 is a schematic, cross sectional view of a reaction
vessel according to an alternative embodiment of the invention.
[0053] FIG. 28 is a partially exploded, isometric view of a
reaction vessel according to another embodiment of the invention in
which the major walls of the reaction chamber are removed to show
the interior of the chamber.
[0054] FIG. 29 is a schematic front view of the vessel of FIG.
28.
[0055] FIG. 30 is a top view of a plunger cap of the vessel of FIG.
28.
[0056] FIG. 31 is a schematic front view of a reaction vessel
according to another embodiment of the invention.
[0057] FIG. 32 is a top view of a plunger cap of the vessel of FIG.
31.
[0058] FIG. 33 is a schematic diagram of a pick-and-place machine
for pressurizing a reaction vessel according to another embodiment
of the invention.
[0059] FIGS. 34-35 are a schematic diagrams of a pick-and-place
machine using a double-bore needle to fill and pressurize a
reaction vessel according to an alternative embodiment of the
invention.
[0060] FIGS. 36-37 are schematic diagrams of a pick-and-place
machine using a single-bore needle to fill and pressurize a
reaction vessel according to another embodiment of the
invention.
[0061] FIGS. 38-39 are schematic diagrams of a press machine having
a platen for sealing a port of a reaction vessel according to an
alternative embodiment of the invention.
DETAILED DESCRIPTION
[0062] The present invention provides an apparatus for thermally
controlling and optically interrogating a reaction mixture, e.g., a
sample mixed with one or more chemicals or reagents. The sample may
also be mixed with diluents or buffers. The sample may be an
aqueous solution containing particles, cells, microorganisms, ions,
or small and large molecules, such as proteins and nucleic acids,
etc. In a particular use, the sample may be a bodily fluid (e.g.,
blood, urine, saliva, sputum, seminal fluid, spinal fluid, mucus,
or other bodily fluids). Alternatively, the sample may be a solid
made soluble in a liquid or the sample may be an environmental
sample such as ground or waste water, soil extracts, pesticide
residues, or airborne spores placed in a liquid.
[0063] In a preferred embodiment, the apparatus includes a reaction
vessel for holding the mixture and a heat-exchanging module into
which the vessel is inserted for thermal processing and optical
detection. The heat-exchanging module includes a pair of opposing
plates between which the vessel is inserted for thermal processing,
one or more heating or cooling elements for heating or cooling the
plates, and optics for optically interrogating the reaction mixture
contained in the vessel. The apparatus also includes a base unit
with processing electronics for receiving a plurality of such
heat-exchanging modules and for independently controlling each
module. The apparatus may also include a controller, such as a
personal computer or network computer, that provides a user
interface to the apparatus and controls the operation of the base
unit. The apparatus is useful for performing heat-exchanging
chemical reactions, such as nucleic acid amplification, and for
optically detecting target analytes.
[0064] FIGS. 1-25 illustrate a preferred embodiment of the
invention. FIG. 1 shows a partially exploded view of a reaction
vessel 12 according to the preferred embodiment, and FIG. 2 shows a
front view of the vessel 12. The vessel 12 includes a reaction
chamber 17 for holding a reaction mixture for thermal processing
and optical interrogation. The vessel 12 is designed for optimal
heat transfer to and from the mixture and for efficient optical
viewing of the mixture. The thin shape of the vessel contributes to
optimal thermal kinetics by providing large surfaces for thermal
conduction. In addition, the side walls of the vessel 12 provide
optical windows into the chamber 17 so that the entire reaction
mixture can be optically interrogated in real-time as the chemical
reaction occurs.
[0065] In more detail to FIGS. 1-2, the reaction vessel 12 includes
a rigid frame 16 that defines the side walls 19A, 19B, 20A, 20B of
the reaction chamber 17. The rigid frame 16 also includes a port 14
and a channel 28 that connects the port 14 to the chamber 17. The
vessel also includes thin, flexible sheets attached to opposite
sides of the rigid frame 16 to form opposing major walls 18 of the
chamber. (The major walls 18 are shown in FIG. 1 exploded from the
rigid frame 16 for illustrative clarity). The reaction chamber 17
is thus defined by the rigid side walls 19A, 19B, 20A, 20B of the
frame 16 and by the flexible major walls 18 which are sealed to
opposite sides of the frame.
[0066] The major walls 18 facilitate optimal thermal conductance to
the reaction mixture contained in the chamber 17. Each of the walls
18 is sufficiently flexible to contact and conform to a respective
thermal surface, thus providing for optimal thermal contact and
heat transfer between the thermal surface and the reaction mixture
contained in the chamber 17. Furthermore, the flexible walls 18
continue to conform to the thermal surfaces if the shape of the
surfaces changes due to thermal expansion or contraction during the
course of the heat-exchanging operation.
[0067] As shown in FIG. 5, the thermal surfaces for contacting the
flexible walls 18 are preferably formed by a pair of opposing
plates 50A, 50B positioned to receive the chamber 17 between them.
When the chamber 17 of the vessel is inserted between the plates
50A, 50B, the inner surfaces of the plates contact the walls 18 and
the flexible walls conform to the surfaces of the plates. The
plates are preferably spaced a distance from each other equal to
the thickness T of the chamber 17 as defined by the thickness of
the frame 16. In this position, minimal or no gaps are found
between the plate surfaces and the walls 18. The plates may be
heated and cooled by various thermal elements to induce temperature
changes within the chamber 17, as is described in greater detail
below.
[0068] The walls 18 are preferably flexible films of polymeric
material such as polypropylene, polyethylene, polyester, or other
polymers. The films may either be layered, e.g., laminates, or the
films may be homogeneous. Layered films are preferred because they
generally have better strength and structural integrity than
homogeneous films. In particular, layered polypropylene films are
presently preferred because polypropylene is not inhibitory to PCR.
Alternatively, the walls 18 may comprise any other material that
may be formed into a thin, flexible sheet and that permits rapid
heat transfer. For good thermal conductance, the thickness of each
wall 18 is preferably between about 0.003 to 0.5 mm, more
preferably between 0.01 to 0.15 mm, and most preferably between
0.025 to 0.08 mm.
[0069] Referring again to FIGS. 1-2, the reaction vessel 12 also
includes a plunger 22 that is inserted into the channel 28 after
filling the chamber 17 with the reaction mixture. The plunger 22
compresses gas in the vessel 12 thereby increasing pressure in the
chamber 17 and outwardly expanding the flexible walls 18. The gas
compressed by the plunger 22 is typically air filling the channel
28. The pressurization of the chamber 17 is important because it
forces the walls 18 against the surfaces of the plates 50A, 50B
(see FIG. 5) and ensures that the walls 18 fully contact and
conform to the inner surfaces of the plates, thus guaranteeing
optimal thermal conductance between the plates 50A, 50B and the
chamber 17.
[0070] Referring again to FIGS. 1-2, the plunger may comprise any
device capable of establishing a seal with the walls of the channel
28 and of compressing gas in the vessel. Such devices include, but
are not limited to, pistons, plugs, or stoppers. The plunger 22 of
the preferred embodiment includes a stem 30 and a piston 32 on the
stem. When the plunger 22 is inserted into the channel 28, the
piston 32 establishes a seal with the inner walls of the channel
and compresses air in the channel. The piston 32 is preferably a
cup integrally formed (e.g., molded) with the stem 30.
Alternatively, the piston 32 may be a separate elastomeric piece
attached to the stem.
[0071] The plunger 22 also preferably includes an alignment ring 34
encircling the stem for maintaining the plunger 22 in coaxial
alignment with the channel 28 as the plunger is inserted into the
channel. The alignment ring 34 is preferably integrally formed
(e.g., molded) with the stem 30. The stem 30 may optionally
includes support ribs 44 for stiffening and strengthening the stem.
The plunger 22 also includes a plunger cap 36 attached to the stem
30. As shown in FIG. 2, the cap 36 includes a snap ring 38 and the
vessel includes an annular recess 23 encircling the port 14 for
receiving the snap ring 38. The cap 36 may optionally include a
lever portion 40 which is lifted to remove the plunger 22 from the
channel 28.
[0072] Referring to FIG. 7A, the rigid frame 16 has an inner
surface 41 defining the channel 28. The inner surface 41 preferably
has one or more pressure control grooves 42 formed therein. In the
preferred embodiment, the inner surface has four pressure control
grooves (only three shown in the view of FIG. 7A) spaced
equidistantly about the circumference of the channel 28. The
pressure control grooves 42 extend from the port 14 to a
predetermined depth D1 in the channel 28. The pressure control
grooves 42 allow gas to escape from the channel 28 and thus prevent
pressurization of the chamber 17 until the piston 32 reaches the
depth D1 in the channel. When the piston 32 reaches the depth D1,
the piston establishes an annular seal with the walls of the
channel 28 and begins to compress air trapped in the channel. The
compression of the trapped air causes the desired pressurization of
the chamber 17.
[0073] The stroke of the plunger 22 into the channel 28 is fully
illustrated in FIGS. 7A-7D. As shown in FIG. 7A, prior to inserting
the plunger 22 into the channel 28, the chamber 17 is filled with
the desired reaction mixture R. Specific methods for filling the
chamber (e.g., pipetting) are discussed in detail below. The
reaction mixture R fills the vessel 12 to a liquid surface level S.
Also prior to inserting the plunger 22 into the channel 28, the
channel 28 contains air having pressure equal to the pressure of
the atmosphere external to the vessel, hereinafter called ambient
pressure. The ambient pressure is usually standard atmospheric
pressure, e.g., about 14.7 pounds per square inch (psi). As shown
in FIG. 7B, when the plunger 22 is first inserted into the channel
28, the piston 32 begins to displace the air in the channel. The
displaced air escapes from the channel 28 through the pressure
control grooves 42.
[0074] Referring now to FIG. 7C, when the piston 32 reaches the
depth D1 at which the pressure control grooves end, the piston 32
establishes an annular seal with the walls of the channel 28 and
begins to compress air trapped in the channel between the piston 32
and the surface level S of the reaction mixture. The reaction
mixture is usually a liquid and therefore substantially
incompressible by the piston. The air trapped in the channel 28,
however, may be compressed to increase pressure in the chamber. As
shown in FIG. 7D, as the plunger 22 is inserted further into the
channel 28, the alignment ring 34 keeps the plunger 22 coaxially
aligned with the channel 28 as the piston 32 continues to compress
air trapped in the channel. When the plunger 22 is fully inserted
in the channel 28, the snap ring 38 snaps into the annular recess
23, ending the plunger stroke.
[0075] When the plunger 22 is fully inserted, the piston 32 seals
the channel 28 at a depth D2 which is lower than the depth D1 at
which the pressure control grooves 42 terminate. The distance D3
traveled by the piston 32 between depths D1 and D2, i.e. the
distance of the pressure stroke, determines the amount of
pressurization of the chamber 17. Referring again to FIG. 5, the
pressure in the chamber 17 should be sufficiently high to ensure
that the flexible major walls 18 of the chamber outwardly expand to
contact and conform to the surfaces of the plates 50A, 50B. The
pressure should not be so great, however, that the flexible walls
18 burst, become unattached from the rigid frame 16, or deform the
frame or plates.
[0076] It is presently preferred to pressurize the chamber to a
pressure in the range of 2 to 50 psi above ambient pressure. This
range is presently preferred because 2 psi is generally enough
pressure to ensure conformity between the flexible walls 18 and the
surfaces of the plates 50A, 50B, while pressures above 50 psi may
cause bursting of the walls 18 or deformation of the frame 16 or
plates 50A, 50B. More preferably, the chamber 17 is pressurized to
a pressure in the range of 8 to 15 psi above ambient pressure. This
range is more preferred because it is safely within the practical
limits described above, i.e. pressures of 8 to 15 psi are usually
more than enough to ensure that the flexible walls 18 contact and
conform to the surfaces of the plates 50A, 50B, but are
significantly lower than the pressures that might burst the walls
18 or deform the frame 16.
[0077] Referring again to FIG. 7D, the desired pressurization of
the chamber 17 may be achieved by proper design of the plunger 22,
channel 28, and pressure control grooves 42 and by use of the
equation:
P.sub.1*V.sub.1=P.sub.2*V.sub.2;
where: P.sub.1 is equal to the pressure in the vessel 12 prior to
insertion of the plunger 22; V.sub.1 is equal to the volume of the
channel 28 between the liquid surface level S and the depth D.sub.1
to which the pressure control grooves 42 extend; P.sub.2 is equal
to the desired final pressure in the chamber 17 after insertion of
the plunger 22 into the channel 28; and V.sub.2 is equal to the
volume of the channel 28 between the liquid surface level S and the
depth D.sub.2 at which the piston 32 establishes a seal with the
walls of the channel 28 when the plunger 22 is fully inserted into
the channel.
[0078] To ensure the desired pressurization P.sub.2 of the chamber
17, one should size the channel 28 and pressure stroke distance
D.sub.3 such that the ratio of the volumes V.sub.1:V.sub.2 is equal
to the ratio of the pressures P.sub.2:P.sub.1. An engineer having
ordinary skill in the art will be able to select suitable values
for the volumes V.sub.1 and V.sub.2 using the description and
equation given above. For example, in the presently preferred
embodiment, the initial pressure P.sub.1 in the vessel is equal to
standard atmospheric pressure of about 14.7 psi, the volume V.sub.1
is equal to 110 .mu.l, the depth D.sub.1 is equal to 0.2 inches,
the depth D.sub.2 is equal to 0.28 inches to give a pressure stroke
distance D.sub.3 of 0.08 inches, and the volume V.sub.2 is equal to
60 .mu.l to give a final pressure P.sub.2 of about 26.7 psi (the
desired 12 psi above ambient pressure). This is just one example of
suitable dimensions for the vessel 12 and is not intended to limit
the scope of the invention. Many other suitable values may be
selected.
[0079] In selecting suitable dimensions for the channel 28 and
pressure stroke distance D.sub.3 (and thus the volumes V.sub.1,
V.sub.2), there is no theoretical limit to how large or small the
dimensions may be. It is only important that the ratio of the
volumes V1:V.sub.2 yield the desired final desired pressure P.sub.2
in the chamber. As a practical matter, however, it is presently
preferred to design the vessel such that the distance D.sub.3 of
the pressure stroke is at least 0.05 inches, i.e., so that the
plunger 22 when fully inserted into the channel 28 extends to a
depth D.sub.2 that is at least 0.05 inches below the depth D.sub.1
at which the pressure control grooves end. This minimum length of
the pressure stroke is preferred to reduce or make negligible the
effect that any manufacturing or operating errors may have on the
pressurization of the chamber. For example, the length of the
pressure stroke may differ slightly from vessel to vessel due to
manufacturing deviations, or the volume of air compressed may vary
due to operator error in filling the vessel (e.g., different fill
levels). If the vessel is designed to have a sufficiently long
pressure stroke, however, such variances will have a lesser or
negligible effect on the ratio of volumes V.sub.1:V.sub.2 and
suitable pressurization of the chamber will still occur. In
addition, to provide a safety margin for manufacturing or operator
errors, one should select a pressure stroke sufficient to achieve a
final pressure P.sub.2 that is safely higher (e.g., at least 3 psi
higher) than the minimum pressure needed to force the flexible
walls of the chamber against the inner surfaces of the plates. With
such a safety margin, any deviations in the final pressure due to
manufacturing deviations or errors in filling the chamber will have
a negligible effect and suitable pressurization of the chamber 17
will still occur. As stated above, the plunger stroke is preferably
designed to increase pressure in the chamber 17 to a pressure in
the range of 8 to 15 psi above ambient pressure to provide the
safety margin.
[0080] The pressure control grooves 42 provide several important
advantages. First, the pressure control grooves 42 provide a simple
mechanism for precisely and accurately controlling the pressure
stroke of the plunger 22, and hence the pressurization of the
chamber 17. Second, the pressure control grooves 42 allow the
plunger 22 to become fully aligned with the channel 28 before the
pressure stroke begins and thus prevent the plunger from becoming
misaligned or cocked in the channel. This ensures a highly
consistent pressure stroke. Although it is possible for the vessel
to have only one pressure control groove, it is preferable for the
vessel to have multiple pressure control grooves (e.g., 2 to 6
grooves) spaced equidistantly about the circumference of the
channel 28. Referring again to FIG. 7A, the pressure control
grooves 42 preferably cut about 0.01 to 0.03 inches into the
surface 41 defining the channel 28. This range is preferred so that
the pressure control grooves 42 are large enough to allow air to
escape from the channel 28, but do not cut so deeply into the
surface 41 that they degrade the structural integrity of the frame
16.
[0081] Although the pressure control grooves 42 are highly
preferred, it is also possible to construct the vessel 12 without
the pressure control grooves and still achieve the desired
pressurization of the chamber 17. One disadvantage of this
embodiment is that the plunger 22 may become misaligned or cocked
in the channel 28 during the pressure stroke so that less
consistent results are achieved. In embodiments in which the vessel
lacks pressure control grooves, the pressure stroke of the plunger
22 begins when the piston 32 enters the channel 28 and establishes
a seal with the walls of the channel. In these embodiments, the
volume V.sub.1 (for use in the equation above) is equal to the
volume of the channel 28 between the liquid surface level S and the
port 14 where the piston 32 first establishes a seal with the walls
of the channel. To ensure the desired pressurization P.sub.2 of the
chamber 17, one should size the channel 28 and length of the
pressure stroke such that the ratio of the volumes V.sub.1:V.sub.2
is equal to the ratio of the pressures P.sub.2:P.sub.1. As
described previously, the minimum length of the pressure stroke is
preferably 0.05 inches to minimize the effect of any manufacturing
or operational deviations.
[0082] Referring again to FIG. 2, the vessel 12 also preferably
includes optical windows for in situ optical interrogation of the
reaction mixture in the chamber 17. In the preferred embodiment,
the optical windows are the side walls 19A, 19B of the rigid frame
16. The side walls 19A, 19B are optically transmissive to permit
excitation of the reaction mixture in the chamber 17 through the
side wall 19A and detection of light emitted from the chamber 17
through the side wall 19B. Arrows A represent illumination beams
entering the chamber 17 through the side wall 19A and arrows B
represent emitted light (e.g., fluorescent emission from labeled
analytes in the reaction mixture) exiting the chamber 17 through
the side wall 19B.
[0083] The side walls 19A, 19B are preferably angularly offset from
each other. It is usually preferred that the walls 19A, 19B are
offset from each other by an angle of about 90.degree.. A
90.degree. angle between excitation and detection paths assures
that a minimum amount of excitation radiation entering through the
wall 19A will exit through wall 19B. In addition, the 90.degree.
angle permits a maximum amount of emitted light, e.g. fluorescence,
to be collected through wall 19B. The walls 19A, 19B are preferably
joined to each other to form a "V" shaped intersection at the
bottom of the chamber 17. Alternatively, the angled walls 19A, 19B
need not be directly joined to each other, but may be separated by
an intermediary portion, such as another wall or various mechanical
or fluidic features which do not interfere with the thermal and
optical performance of the vessel. For example, the walls 19A, 19B
may meet at a port which leads to another processing area in
communication with the chamber 17, such as an integrated capillary
electrophoresis area. In the presently preferred embodiment, a
locating tab 27 extends from the frame 16 below the intersection of
walls 19A, 19B. The locating tab 27 is used to properly position
the vessel 12 in a heat-exchanging module described below with
reference to FIG. 8.
[0084] Optimum optical sensitivity may be attained by maximizing
the optical path length of the light beams exciting the labeled
analytes in the reaction mixture and the emitted light that is
detected, as represented by the equation:
I.sub.o/I.sub.i=C*L*A,
where I.sub.o is the illumination output of the emitted light in
volts, photons or the like, C is the concentration of analyte to be
detected, I.sub.i is the input illumination, L is the path length,
and A is the intrinsic absorptivity of the dye used to label the
analyte.
[0085] The thin, flat reaction vessel 12 of the present invention
optimizes detection sensitivity by providing maximum optical path
length per unit analyte volume. Referring to FIGS. 4-5, the vessel
12 is preferably constructed such that each of the sides walls 19A,
19B, 20A, 20B of the chamber 17 has a length L in the range of 1 to
15 mm, the chamber has a width W in the range of 1.4 to 20 mm, the
chamber has a thickness T in the range of 0.5 to 5 mm, and the
ratio of the width W of the chamber to the thickness T of the
chamber is at least 2:1. These parameters are presently preferred
to provide a vessel having a relatively large average optical path
length through the chamber, i.e. 1 to 15 mm on average, while still
keeping the chamber sufficiently thin to allow for extremely rapid
heating and cooling of the reaction mixture contained therein. The
average optical path length of the chamber 17 is the distance from
the center of the side wall 19A to the center of the chamber 17
plus the distance from the center of the chamber 17 to the center
of the side wall 19B. As used herein, the thickness T of the
chamber 17 is defined as the thickness of the chamber prior to the
outward expansion of the major walls, i.e. the thickness T of the
chamber is defined by the thickness of the frame 16.
[0086] More preferably, the vessel 12 is constructed such that each
of the sides walls 19A, 19B, 20A, 20B of the chamber 17 has a
length L in the range of 5 to 12 mm, the chamber has a width W in
the range of 7 to 17 mm, the chamber has a thickness T in the range
of 0.5 to 2 mm, and the ratio of the width W of the chamber to the
thickness T of the chamber is at least 4:1. These ranges are more
preferable because they provide a vessel having both a larger
average optical path length (i.e., 5 to 12 mm) and a volume
capacity in the range of 12 to 100 .mu.l while still maintaining a
chamber sufficiently thin to permit extremely rapid heating and
cooling of a reaction mixture. The relatively large volume capacity
provides for increased sensitivity in the detection of low
concentration analytes, such as nucleic acids.
[0087] In the preferred embodiment, the reaction vessel 12 has a
diamond-shaped chamber 17 defined by the side walls 19A, 19B, 20A,
20B, each of the side walls has a length of about 10 mm, the
chamber has a width of about 14 mm, the chamber has a thickness T
of 1 mm as defined by the thickness of the frame 16, and the
chamber has a volume capacity of about 100 .mu.l. This reaction
vessel provides a relatively large average optical path length of
10 mm through the chamber 17. Additionally, the thin chamber allows
for extremely rapid heating and/or cooling of the reaction mixture
contained therein. The diamond-shape of the chamber 17 helps
prevent air bubbles from forming in the chamber as it is filled
with the reaction mixture and also aids in optical interrogation of
the mixture.
[0088] The frame 16 is preferably made of an optically transmissive
material, e.g., a polycarbonate or clarified polypropylene, so that
the side walls 19A, 19B are optically transmissive. As used herein,
the term optically transmissive means that one or more wavelengths
of light may be transmitted through the walls. In the preferred
embodiment, the optically transmissive walls 19A, 19B are
substantially transparent. In addition, one or more optical
elements may be present on the optically transmissive side walls
19A, 19B. The optical elements may be designed, for example, to
maximize the total volume of solution which is illuminated by a
light source, to focus excitation light on a specific region of the
chamber 17, or to collect as much fluorescence signal from as large
a fraction of the chamber volume as possible. In alternative
embodiments, the optical elements may comprise gratings for
selecting specific wavelengths, filters for allowing only certain
wavelengths to pass, or colored lenses to provide filtering
functions. The wall surfaces may be coated or comprise materials
such as liquid crystal for augmenting the absorption of certain
wavelengths. In the presently preferred embodiment, the optically
transmissive walls 19A, 19B are substantially clear, flat windows
having a thickness of about 1 mm.
[0089] As shown in FIG. 2, the side walls 20A, 20B preferably
includes reflective faces 21 which internally reflect light trying
to exit the chamber 17 through the side walls 20A, 20B. The
reflective faces 21 are arranged such that adjacent faces are
angularly offset from each other by about 90.degree.. In addition,
the frame 16 defines open spaces between the side walls 20A, 20B
and support ribs 15. The open spaces are occupied by ambient air
that has a different refractive index than the material composing
the frame (e.g., plastic). Due to the difference in the refractive
indexes, the reflective faces 21 are effective for internally
reflecting light trying to exit the chamber through the walls 20A,
20B and provide for increased detection of optical signal through
the walls 19A, 19B. In the preferred embodiment, the optically
transmissive side walls 19A, 19B define the bottom portion of the
diamond-shaped chamber 17, and the retro-reflective side walls 20A,
20B define the top portion of the chamber.
[0090] The reaction vessel 12 may be used in manual operations
performed by human technicians or in automated operations performed
by machines, e.g. pick-and-place machines. As shown in FIG. 1, for
the manual embodiments, the vessel 12 preferably includes finger
grips 26 and a leash 24 that conveniently attaches the plunger 22
to the body of the vessel 12. As shown in FIG. 3, for automated
embodiments, the plunger cap 36 preferably includes a tapered
engagement aperture 46 for receiving and establishing a fit with a
robotic arm or machine tip (not shown in FIG. 3), thus enabling the
machine tip to pick and place the plunger in the channel. The
engagement aperture 46 preferably has tapered side walls for
establishing a friction fit with the machine tip. Alternatively,
the engagement aperture may be designed to establish a vacuum fit
with the machine tip. The plunger cap 36 may optionally include
alignment apertures 48A, 48B used by the machine tip to properly
align the plunger cap 36 as the plunger is inserted into the
channel, as is described in greater detail below with reference to
FIG. 25.
[0091] A preferred method for fabricating the reaction vessel 12
will now be described with reference to FIGS. 1-2. The reaction
vessel 12 may be fabricated by first molding the rigid frame 16
using known injection molding techniques. The frame 16 is
preferably molded as a single piece of polymeric material, e.g.,
clarified polypropylene. After the frame 16 is produced, thin,
flexible sheets are cut to size and sealed to opposite sides of the
frame 16 to form the major walls 18 of the chamber 17.
[0092] The major walls 18 are preferably cast or extruded films of
polymeric material, e.g., polypropylene films, that are cut to size
and attached to the frame 16 using the following procedure. A first
piece of film is placed over one side of the bottom portion of the
frame 16. The frame 16 preferably includes a tack bar 47 for
aligning the top edge of the film. The film is placed over the
bottom portion of the frame 16 such that the top edge of the film
is aligned with the tack bar 47 and such that the film completely
covers the bottom portion of the frame 16 below the tack bar 47.
The film should be larger than the bottom portion of the frame 16
so that it may be easily held and stretched flat across the frame.
The film is then cut to size to match the outline of the frame by
clamping to the frame the portion of the film that covers the frame
and cutting away the portions of the film that extend past the
perimeter of the frame using, e.g., a laser or die. The film is
then tack welded to the frame, preferably using a laser.
[0093] The film is then sealed to the frame 16, preferably by heat
sealing. Heat sealing is presently preferred because it produces a
strong seal without introducing potential contaminants to the
vessel as the use of adhesive or solvent bonding techniques might
do. Heat sealing is also simple and inexpensive. At a minimum, the
film should be completely sealed to the surfaces of the side walls
19A, 19B, 20A, 20B. More preferably, the film is additionally
sealed to the surfaces of the support ribs 15 and tack bar 47. The
heat sealing may be performed using, e.g., a heated platen. An
identical procedure may be used to cut and seal a second sheet to
the opposite side of the frame 16 to complete the chamber 17.
[0094] Many variations to this fabrication procedure are possible.
For example, in an alternative embodiment, the film is stretched
across the bottom portion of the frame 16 and then sealed to the
frame prior to cutting the film to size. After sealing the film to
the frame, the portions of the film that extend past the perimeter
of the frame are cut away using, e.g., a laser or die.
[0095] The plunger 22 is also preferably molded from polymeric
material, preferably polypropylene, using known injection molding
techniques. As shown in FIG. 1, the frame 16, plunger 22, and leash
24 connecting the plunger to the frame may all be formed in the
same mold to form a one-piece part. This embodiment of the vessel
is especially suitable for manual use in which a human operator
fills the vessel and inserts the plunger 22 into the channel 28.
The leash 24 ensures that the plunger 22 is not lost or dropped on
the floor. Alternatively, as shown in FIG. 2, the plunger 22 may be
molded separately from the frame 16 so that the plunger and frame
are separate pieces. This embodiment is especially suitable for
automated use of the vessel in which the plunger 22 is picked and
placed into the channel 28 by an automated machine.
[0096] Although it is presently preferred to mold the frame 16 as a
single piece, it is also possible to fabricate the frame from
multiple pieces. For example, the side walls 19A, 19B forming the
angled optical windows may be molded from polycarbonate, which has
good optical transparency, while the rest of the frame is molded
from polypropylene, which is inexpensive and compatible with PCR.
The separate pieces can be attached together in a secondary step.
For example, the side walls 19A, 19B may be press-fitted and/or
bonded to the remaining portion of the frame 16. The flexible walls
18 may then be attached to opposite sides of the frame 16 as
previously described.
[0097] Referring again to FIG. 5, the plates 50A, 50B may be made
of various thermally conductive materials including ceramics or
metals. Suitable ceramic materials include aluminum nitride,
aluminum oxide, beryllium oxide, and silicon nitride. Other
materials from which the plates may be made include, e.g., gallium
arsenide, silicon, silicon nitride, silicon dioxide, quartz, glass,
diamond, polyacrylics, polyamides, polycarbonates, polyesters,
polyimides, vinyl polymers, and halogenated vinyl polymers, such as
polytetrafluoroethylenes. Other possible plate materials include
chrome/aluminum, superalloys, zircaloy, aluminum, steel, gold,
silver, copper, tungsten, molybdenum, tantalum, brass, sapphire, or
any of the other numerous ceramic, metal, or polymeric materials
available in the art.
[0098] Ceramic plates are presently preferred because their inside
surfaces may be conveniently machined to very high smoothness for
high wear resistance, high chemical resistance, and good thermal
contact to the flexible walls of the reaction vessel. Ceramic
plates can also be made very thin, preferably between about 0.6 and
1.3 mm, for low thermal mass to provide for extremely rapid
temperature changes. A plate made from ceramic is also both a good
thermal conductor and an electrical insulator, so that the
temperature of the plate may be well controlled using a resistive
heating element coupled to the plate.
[0099] Various thermal elements may be employed to heat and/or cool
the plates 50A, 50B and thus control the temperature of the
reaction mixture in the chamber 17. In general, suitable heating
elements for heating the plate include conductive heaters,
convection heaters, or radiation heaters. Examples of conductive
heaters include resistive or inductive heating elements coupled to
the plates, e.g., resistors or thermoelectric devices.
[0100] Suitable convection heaters include forced air heaters or
fluid heat-exchangers for flowing fluids past the plates. Suitable
radiation heaters include infrared or microwave heaters. Similarly,
various cooling elements may be used to cool the plates. For
example, various convection cooling elements may be employed such
as a fan, peltier device, refrigeration device, or jet nozzle for
flowing cooling fluids past the surfaces of the plates.
Alternatively, various conductive cooling elements may be used,
such as a heat sink, e.g. a cooled metal block, in direct contact
with the plates.
[0101] Referring to FIG. 6, in the preferred embodiment, each plate
50 has a resistive heating element 56 disposed on its outer
surface. The resistive heating element 56 is preferably a thick or
thin film and may be directly screen printed onto each plate 50,
particularly plates comprising a ceramic material, such as aluminum
nitride or aluminum oxide. Screen-printing provides high
reliability and low cross-section for efficient transfer of heat
into the reaction chamber. Thick or thin film resistors of varying
geometric patterns may be deposited on the outer surfaces of the
plates to provide more uniform heating, for example by having
denser resistors at the extremities and thinner resistors in the
middle. Although it is presently preferred to deposit a heating
element on the outer surface of each plate, a heating element may
alternatively be baked inside of each plate, particularly if the
plates are ceramic. The heating element 56 may comprise metals,
tungsten, polysilicon, or other materials that heat when a voltage
difference is applied across the material.
[0102] The heating element 56 has two ends which are connected to
respective contacts 54 which are in turn connected to a voltage
source (not shown in FIG. 6) to cause a current to flow through the
heating element. Each plate 50 also preferably includes a
temperature sensor 52, such as a thermocouple, thermistor, or RTD,
which is connected by two traces 53 to respective contacts 54. The
temperature sensor 52 may be used to monitor the temperature of the
plate 50 in a controlled feedback loop.
[0103] It is important that the plates have a low thermal mass to
enable rapid heating and cooling of the plates. In particular, it
is presently preferred that each of the plates has a thermal mass
less than about 5 J/.degree. C., more preferably less than 3
J/.degree. C., and most preferably less than 1 J/.degree. C. As
used herein, the term thermal mass of a plate is defined as the
specific heat of the plate multiplied by the mass of the plate. In
addition, each plate should be large enough to cover a respective
major wall of the reaction chamber. In the presently preferred
embodiment, for example, each of the plates has a width X in the
range of 2 to 22 mm, a length Y in the range of 2 to 22 mm, and a
thickness in the range of 0.5 to 5 mm. The width X and length Y of
each plate is selected to be slightly larger than the width and
length of the reaction chamber. Moreover, each plate preferably has
an angled bottom portion matching the geometry of the bottom
portion of the reaction chamber, as is described below with
reference to FIG. 12. Also in the preferred embodiment, each of the
plates is made of aluminum nitride having a specific heat of about
0.75 J/g.degree. C. The mass of each plate is preferably in the
range of 0.005 to 5.0 g so that each plate has a thermal mass in
the range of 0.00375 to 3.75 J/.degree. C.
[0104] FIG. 8 is a schematic side view of a heat-exchanging module
60 into which the reaction vessel 12 is inserted for thermal
processing and optical interrogation. The module 60 preferably
includes a housing 62 for holding the various components of the
module. The module 60 also includes the thermally conductive plates
50 described above. The housing 62 includes a slot (not shown in
FIG. 8) above the plates 50 so that the reaction chamber of the
vessel 12 may be inserted through the slot and between the plates.
The heat-exchanging module 60 also preferably includes a cooling
system, such as a fan 66. The fan 66 is positioned to blow cooling
air past the surfaces of the plates 50 to cool the plates and hence
cool the reaction mixture in the vessel 12. The housing 62
preferably defines channels for directing the cooling air past the
plates 50 and out of the module 60.
[0105] The heat-exchanging module 60 further includes an optical
excitation assembly 68 and an optical detection assembly 70 for
optically interrogating the reaction mixture contained in the
vessel 12. The excitation assembly 68 includes a first circuit
board 72 for holding its electronic components, and the detection
assembly 68 includes a second circuit board 74 for holding its
electronic components. The excitation assembly 68 includes one or
more light sources, such as LEDs, for exciting
fluorescently-labeled analytes in the vessel 12. The excitation
assembly 68 also includes one or more lenses for collimating the
light from the light sources, as well as filters for selecting the
excitation wavelength ranges of interest. The detection assembly 70
includes one or more detectors, such as photodiodes, for detecting
the light emitted from the vessel 12. The detection assembly 70
also includes one or more lenses for focusing and collimating the
emitted light, as well as filters for selecting the emission
wavelength ranges of interest. The specific components of the
optics assemblies 68, 70 are described in greater detail below with
reference to FIGS. 16-19.
[0106] The optics assemblies 68, 70 are positioned in the housing
62 such that when the chamber of the vessel 12 is inserted between
the plates 50, the first optics assembly 68 is in optical
communication with the chamber 17 through the optically
transmissive side wall 19A (see FIG. 2) and the second optics
assembly 70 is in optical communication with the chamber through
the optically transmissive side wall 19B (FIG. 2). In the preferred
embodiment, the optics assemblies 68, 70 are placed into optical
communication with the optically transmissive side walls by simply
locating the optics assemblies 68, 70 next to the bottom edges of
the plates 50 so that when the chamber of the vessel is placed
between the plates, the optics assemblies 68, 70 directly contact,
or are in close proximity to, the side walls.
[0107] As shown in FIG. 12, the vessel 12 preferably has an angled
bottom portion (e.g., triangular) formed by the optically
transmissive side walls 19A, 19B. Each of the plates 50A, 50B has a
correspondingly shaped bottom portion. The bottom portion of the
first plate 50A has a first bottom edge 98A and a second bottom
edge 98B. Similarly, the bottom portion of the second plate 50B has
a first bottom edge 99A and a second bottom edge 99B. The first and
second bottom edges of each plate are preferably angularly offset
from each other by the same angle that the side walls 19A, 19B are
offset from each other (e.g., 90.degree.). Additionally, the plates
50A, 50B are preferably positioned to receive the chamber of the
vessel 12 between them such that the first side wall 19A is
positioned substantially adjacent and parallel to each of the first
bottom edges 98A, 99A and such that the second side wall 19B is
positioned substantially adjacent and parallel to each of the
second bottom edges 98B, 99B. This arrangement provides for easy
optical access to the optically transmissive side walls 19A, 19B
and hence to the chamber of the vessel 12.
[0108] The side walls 19A, 19B may be positioned flush with the
edges of the plates 50A, 50B, or more preferably, the side walls
19A, 19B may be positioned such that they protrude slightly past
the edges of the plates. As is explained below with reference to
FIGS. 16-19, each optics assembly preferably includes a lens that
physically contacts a respective one of the side walls 19A, 19B. It
is preferred that the side walls 19A, 19B protrude slightly (e.g.,
0.02 to 0.3 mm) past the edges of the plates 50A, 50B so that the
plates do not physically contact and damage the lenses. A gel or
fluid may optionally be used to establish or improve optical
communication between each optics assembly and the side walls 19A,
19B. The gel or fluid should have a refractive index close to the
refractive indexes of the elements that it is coupling.
[0109] Referring again to FIG. 8, the optics assemblies 68, 70 are
preferably arranged to provide a 90.degree. angle between
excitation and detection paths. The 90.degree. angle between
excitation and detection paths assures that a minimum amount of
excitation radiation entering through the first side wall of the
chamber exits through the second side wall. Also, the 90.degree.
angle permits a maximum amount of emitted radiation to be collected
through the second side wall. In the preferred embodiment, the
vessel 12 includes a locating tab 27 (see FIG. 2) that fits into a
slot formed between the optics assemblies 68, 70 to ensure proper
positioning of the vessel 12 for optical detection. For improved
detection, the module 60 also preferably includes a light-tight lid
(not shown) that is placed over the top of the vessel 12 and made
light-tight to the housing 62 after the vessel is inserted between
the plates 50.
[0110] Although it is presently preferred to locate the optics
assemblies 68, 70 next to the bottom edges of the plates 50, many
other arrangements are possible. For example, optical communication
may be established between the optics assemblies 68, 70 and the
walls of the vessel 12 via optical fibers, light pipes, wave
guides, or similar devices. One advantage of these devices is that
they eliminate the need to locate the optics assemblies 68, 70
physically adjacent to the plates 50. This leaves more room around
the plates in which to circulate cooling air or refrigerant, so
that cooling may be improved.
[0111] The heat-exchanging module 60 also includes a PC board 76
for holding the electronic components of the module and an edge
connector 80 for connecting the module 60 to a base instrument, as
will be described below with reference to FIG. 22. The heating
elements and temperature sensors on the plates 50, as well as the
optical boards 72, 74, are connected to the PC board 76 by flex
cables (not shown in FIG. 8 for clarity of illustration). The
module 60 may also include a grounding trace 78 for shielding the
optical detection circuit. The module 60 also preferably includes
an indicator, such as an LED 64, for indicating to a user the
current status of the module such as "ready to load sample", "ready
to load reagent," "heating," "cooling," "finished," or "fault".
[0112] The housing 62 may be molded from a rigid, high-performance
plastic, or other conventional material. The primary functions of
the housing 62 are to provide a frame for holding the plates 50,
optics assemblies 68, 70, fan 66, and PC board 76. The housing 62
also preferably provides flow channels and ports for directing
cooling air from the fan 66 across the surfaces of the plates 50
and out of the housing. In the preferred embodiment, the housing 62
comprises complementary pieces (only one piece shown in the
schematic side view of FIG. 8) that fit together to enclose the
components of the module 60 between them.
[0113] The opposing plates 50 are positioned to receive the chamber
of the vessel 12 between them such that the flexible major walls of
the chamber contact and conform to the inner surfaces of the
plates. It is presently preferred that the plates 50 be held in an
opposing relationship to each other using, e.g., brackets,
supports, or retainers. Alternatively, the plates 50 may be
spring-biased towards each other as described in International
Publication Number WO 98/38487, the disclosure of which is
incorporated by reference herein. In another embodiment of the
invention, one of the plates is held in a fixed position, and the
second plate is spring-biased towards the first plate. If one or
more springs are used to bias the plates towards each other, the
springs should be sufficiently stiff to ensure that the plates are
pressed against the flexible walls of the vessel with sufficient
force to cause the walls to conform to the inner surfaces of the
plates.
[0114] FIGS. 9-10 illustrate a preferred support structure 81 for
holding the plates 50A, 50B in an opposing relationship to each
other. FIG. 9 shows an exploded view of the structure, and FIG. 10
shows an assembled view of the structure. For clarity of
illustration, the support structure 81 and plates 50A, 50B are
shown upside down relative to their normal orientation in the
heat-exchanging module of FIG. 8. Referring to FIG. 9, the support
structure 81 includes a mounting plate 82 having a slot 83 formed
therein. The slot 83 is sufficiently large to enable the chamber of
the vessel to be inserted through it. Spacing posts 84A, 84B extend
from the mounting plate 82 on opposite sides of the slot 83.
Spacing post 84A has indentations 86 formed on opposite sides
thereof (only one side visible in the isometric view of FIG. 9),
and spacing post 84B has indentations 87 formed on opposite sides
thereof (only one side visible in the isometric view of FIG. 9).
The indentations 86, 87 in the spacing posts are for receiving the
edges of the plates 50A, 50B. To assemble the structure, the plates
50A, 50B are placed against opposite sides of the spacing posts
84A, 84B such that the edges of the plates are positioned in the
indentations 86, 87. The edges of the plates are then held in the
indentations using a suitable retention means. In the preferred
embodiment, the plates are retained by retention clips 88A, 88B.
Alternatively, the plates 50A, 50B may be retained by adhesive
bonds, screws, bolts, clamps, or any other suitable means.
[0115] The mounting plate 82 and spacing posts 84A, 84B are
preferably integrally formed as a single molded piece of plastic.
The plastic should be a high temperature plastic, such as
polyetherimide, which will not deform of melt when the plates 50A,
50B are heated. The retention clips 84A, 84B are preferably
stainless steel. The mounting plate 82 may optionally include
indentations 92A, 92B for receiving flex cables 90A, 90B,
respectively, that connect the heating elements and temperature
sensors disposed on the plates 50A, 50B to the PC board 76 of the
heat-exchanging module 60 (FIG. 8). The portion of the flex cables
90A adjacent the plate 50A is held in the indentation 92A by a
piece of tape 94A, and the portion of the flex cables 90B adjacent
the plate 50B is held in the indentation 92B by a piece of tape
94B.
[0116] FIG. 11 is an isometric view of the assembled support
structure 81. The mounting plate 82 preferably includes tabs 96
extending from opposite sides thereof for securing the structure 81
to the housing of the heat-exchanging module. Referring again to
FIG. 8, the housing 62 preferably includes slots for receiving the
tabs to hold the mounting plate 82 securely in place.
Alternatively, the mounting plate 82 may be attached to the housing
62 using, e.g., adhesive bonding, screws, bolts, clamps, or any
other conventional means of attachment.
[0117] Referring again to FIG. 9, the support structure 81
preferably holds the plates 50A, 50B so that their inner surfaces
are angled very slightly towards each other. In the preferred
embodiment, each of the spacing posts 84A, 84B has a wall 89 that
is slightly tapered so that when the plates 50A, 50B are pressed
against opposite sides of the wall, the inner surfaces of the
plates are angled slightly towards each other. As best shown in
FIG. 5, the inner surfaces of the plates 50A, 50B angle towards
each other to form a slightly V-shaped slot into which the chamber
17 is inserted. The amount by which the inner surfaces are angled
towards each other is very slight, preferably about 1.degree. from
parallel. The surfaces are angled towards each other so that, prior
to the insertion of the chamber 17 between the plates 50A, 50B, the
bottoms of the plates are slightly closer to each other than the
tops. This slight angling of the inner surfaces enables the chamber
17 of the vessel to be inserted between the plates and withdrawn
from the plates more easily. Alternatively, the inner surfaces of
the plates 50A, 50B could be held parallel to each other, but
insertion and removal of the vessel 12 would be more difficult.
[0118] In addition, the inner surfaces of the plates 50A, 50B are
preferably spaced from each other a distance equal to the thickness
of the frame 16. In embodiments in which the inner surfaces are
angled towards each other, the centers of the inner surfaces are
preferably spaced a distance equal to the thickness of the frame 16
and the bottoms of the plates are initially spaced a distance that
is slightly less than the thickness of the frame 16. When the
chamber 17 is inserted between the plates 50A, 50B, the rigid frame
16 forces the bottom portions of the plates apart so that the
chamber 17 is firmly sandwiched between the plates. The distance
that the plates 50A, 50B are wedged apart by the frame 16 is
usually very small, e.g., about 0.035 mm if the thickness of the
frame is 1 mm and the inner surfaces are angled towards each other
by 1.degree..
[0119] Referring again to FIG. 10, the retention clips 88A, 88B
should be sufficiently flexible to accommodate this slight outward
movement of the plates 50A, 50B, yet sufficiently stiff to hold the
plates within the recesses in the spacing posts 84A, 84B during
insertion and removal of the vessel. The wedging of the vessel
between the plates 50A, 50B provides an initial preload against the
chamber and ensures that the flexible major walls of the chamber,
when pressurized, establish good thermal contact with the inner
surfaces of the plates.
[0120] Referring again to FIG. 8, to limit the amount that the
plates 50 can spread apart due to the pressurization of the vessel
12, stops may be molded into the housings of optics assemblies 68,
70. As shown in FIG. 13, the housing 221 of the optics assembly 70
includes claw-like stops 247A, 247B that extend outwardly from the
housing. As shown in FIG. 14, the housing 221 is positioned such
that the bottom edges of the plates 50A, 50B are inserted between
the stops 247A, 247B. The stops 247A, 247B thus prevent the plates
50A, 50B from spreading farther than a predetermined maximum
distance from each other. Although not shown in FIG. 14 for
illustrative clarity, the optics assembly 68 (see FIG. 8) has a
housing with corresponding stops for preventing the other halves of
the plates from spreading farther than the predetermined maximum
distance from each other. Referring again to FIG. 14, the maximum
distance that stops 247A, 247B permit the inner surfaces of the
plates 50A, 50B to be spaced from each other should closely match
the thickness of the frame 16. Preferably, the maximum spacing of
the inner surfaces of the plates 50A, 50B is slightly larger than
the thickness of the frame 16 to accommodate tolerance variations
in the vessel 12 and plates 50A, 50B. For example, the maximum
spacing is preferably about 0.1 to 0.3 mm greater than the
thickness of the frame 16.
[0121] FIGS. 15A and 15B show the fluorescent excitation and
emission spectra, respectively, of four fluorescent dyes of
interest. These dyes are standard fluorescent dyes used with the
TaqMan.RTM. chemistry (available from the Perkin-Elmer Corporation,
Foster City, Calif.) and are well known by their acronyms FAM, TET,
TAMRA, and ROX. Although the preferred embodiment is described with
reference to these four dyes, it is to be understood that the
apparatus of the present invention is not limited to these
particular dyes or to the TaqMan.RTM. chemistry. The apparatus may
be used with any fluorescent dyes or with interculating dyes such
as SYBRGreen.TM. or ethidium bromide. Such dyes are commercially
available from various well known suppliers. Fluorescent dyes and
labeling chemistries for labeling analytes in a reaction mixture
are well known in the art and need not be discussed further herein.
Further, although fluorescence detection is presently preferred,
the apparatus of the present invention is not limited to detection
based upon fluorescent labels. The apparatus may be applicable to
detection based upon phosphorescent labels, chemiluminescent
labels, or electrochemiluminescent labels.
[0122] As shown in FIG. 15A, the excitation spectra curves for FAM,
TET, TAMRA, and ROX are typically very broad at the base, but
sharper at the peaks. As shown in FIG. 15B, the relative emission
spectra curves for the same dyes are also very broad at the base
and sharper at the peaks. Thus, these dyes have strongly
overlapping characteristics in both their excitation and emission
spectra. The overlapping characteristics have traditionally made it
difficult to distinguish the fluorescent signal of one dye from
another when multiple dyes are used to label different analytes in
a reaction mixture.
[0123] According to the present invention, multiple light sources
are used to provide excitation beams to the dyes in multiple
excitation wavelength ranges. Each light source provides excitation
light in a wavelength range matched to the peak excitation range of
a respective one of the dyes. In the preferred embodiment, the
light sources are blue and green LEDs. FIG. 15C shows the effects
of filtering the outputs of blue and green LEDs to provide
substantially distinct excitation wavelength ranges. Typical blue
and green LEDs have substantial overlap in the range of around 480
nm through 530 nm. By the filtering regime of the present
invention, the blue LED light is filtered to a range of about 450
to 495 nm to match the relative excitation peak for FAM. The green
LED light is filtered to a first range of 495 to 527 nm
corresponding to the excitation peak for TET, a second range of 527
to 555 nm corresponding to the excitation peak for TAMRA, and a
third range of 555 to 593 nm corresponding to the excitation peak
for ROX.
[0124] FIG. 15D shows the effects of filtering light emitted
(fluorescent emission) from each of the four dyes to form distinct
emission wavelength ranges. As shown previously in FIG. 15B, the
fluorescent emissions of the dyes before filtering are spherically
diffuse with overlapping spectral bandwidths, making it difficult
to distinguish the fluorescent output of one dye from another. As
shown in FIG. 15D, by filtering the fluorescent emissions of the
dyes into substantially distinct wavelength ranges, a series of
relatively narrow peaks (detection windows) are obtained, making it
possible to distinguish the fluorescent outputs of different dyes,
thus enabling the detection of a number of different
fluorescently-labeled analytes in a reaction mixture.
[0125] FIG. 16 is a schematic, plan view of the optical excitation
assembly 68. The assembly 68 is positioned adjacent the reaction
vessel 12 to transmit excitation beams to the reaction mixture
contained in the chamber 17. FIG. 17 is an exploded view of the
excitation assembly. As shown in FIGS. 16-17, the excitation
assembly 68 includes a housing 219 for holding various components
of the assembly. The housing 219 includes stops 245A, 245B for
limiting the maximum spacing of the thermal plates, as previously
discussed with reference to FIGS. 8 and 14. The housing 219
preferably comprises one or more molded pieces of plastic. In the
preferred embodiment, the housing 219 is a multi-part housing
comprised of three housing elements 220A, 220B, and 220C. The upper
and lower housing elements 220A and 220C are preferably
complementary pieces that couple together and snap-fit into housing
element 220B. In this embodiment, the housing elements 220A and
220C are held together by screws 214. In alternative embodiments,
the entire housing 219 may be a one-piece housing that holds a
slide-in optics package.
[0126] The lower housing element 220C includes an optical window
235 into which is placed a cylindrical rod lens 215 for focusing
excitation beams into the chamber 17. In general, the optical
window 235 may simply comprise an opening in the housing through
which excitation beams may be transmitted to the chamber 17. The
optical window may optionally include an optically transmissive or
transparent piece of glass or plastic serving as a window pane, or
as in the preferred embodiment, a lens for focusing excitation
beams. The lens 215 preferably directly contacts one of the
optically transmissive side walls of the chamber 17.
[0127] The optics assembly 68 also includes four light sources,
preferably LEDs 100A, 100B, 100C, and 100D, for transmitting
excitation beams through the lens 215 to the reaction mixture
contained in the chamber 17. In general, each light source may
comprise a laser, a light bulb, or an LED. In the preferred
embodiment, each light source comprises a pair of directional LEDs.
In particular, the four light sources shown in FIGS. 16-17 are
preferably a first pair of green LEDs 100A, a second pair of green
LEDs 100B, a pair of blue LEDs 100C, and a third pair of green LEDs
100D. The LEDs receive power through leads 201 which are connected
to a power source (not shown in FIGS. 16-17). The LEDs are mounted
to the optical circuit board 72 which is attached to the back of
the housing element 220B so that the LEDs are rigidly fixed in the
housing. The optical circuit board 72 is connected to the main PC
board of the heat-exchanging module (shown in FIG. 8) via the flex
cable 103.
[0128] The optics assembly 68 further includes a set of filters and
lenses arranged in the housing 219 for filtering the excitation
beams generated by the LEDs so that each of the beams transmitted
to the chamber 17 has a distinct excitation wavelength range. As
shown in FIG. 17, the lower housing element 220C preferably
includes walls 202 that create separate excitation channels in the
housing to reduce potential cross-talk between the different pairs
of LEDs. The walls 202 preferably include slots for receiving and
rigidly holding the filters and lenses. The filters and lenses may
also be fixed in the housing by means of an adhesive used alone, or
more preferably, with an adhesive used in combination with slots in
the housing.
[0129] Referring to FIG. 16, the filters in the optics assembly 68
may be selected to provide excitation beams to the reaction mixture
in the chamber 17 in any desired excitation wavelength ranges. The
optics assembly 68 may therefore be used with any fluorescent,
phosphorescent, chemiluminescent, or electrochemiluminescent labels
of interest. For purposes of illustration, one specific embodiment
of the assembly 68 will now be described in which the assembly is
designed to provide excitation beams corresponding to the peak
excitation wavelength ranges FAM, TAMRA, TET, and ROX.
[0130] In this embodiment, a pair of 593 nm low pass filters 203
are positioned in front of green LEDs 100A, a pair of 555 nm low
pass filters 204 are positioned in front of green LEDs 100B, a pair
of 495 nm low pass filters 205 are positioned in front of blue LEDs
100C, and a pair of 527 nm low pass filters 206 are positioned in
front of green LEDs 100D. Although it is presently preferred to
position a pair of low pass filters in front of each pair of LEDs
for double filtering of excitation beams, a single filter may be
used in alternative embodiments. In addition, a lens 207 is
preferably positioned in front of each pair of filters for
collimating the filtered excitation beams. The optics assembly 68
also includes a 495 nm high pass reflector 208, a 527 nm high pass
reflector 209, a mirror 210, a 555 nm low pass reflector 211, and a
593 nm low pass reflector 212. The reflecting filters and mirrors
208-212 are angularly offset by 30.degree. from the low pass
filters 203-206.
[0131] The excitation assembly 68 transmits excitation beams to the
chamber 17 in four distinct excitation wavelength ranges as
follows. When the green LEDs 100A are activated, they generate an
excitation beam that passes through the pair of 593 nm low pass
filters 203 and through the lens 207. The excitation beam then
reflects off of the 593 nm low pass reflector 212, passes through
the 555 nm low pass reflector 211, reflects off of the 527 nm high
pass reflector 209, and passes through the lens 215 into the
reaction chamber 17.
[0132] The excitation beam from the LEDs 100A is thus filtered to a
wavelength range of 555 to 593 nm corresponding to the peak
excitation range for ROX. When the green LEDs 100B are activated,
they generate an excitation beam that passes through the pair of
555 nm low pass filters 204, reflects off of the 555 nm low pass
reflector 211, reflects off of the 527 nm high pass reflector 209,
and passes through the lens 215 into the reaction chamber 17. The
excitation beam from LEDs 100B is thus filtered to a wavelength
range of 527 to 555 nm corresponding to the peak excitation range
for TAMRA.
[0133] When the blue LEDs 100C are activated, they generate an
excitation beam that passes through the pair of 495 nm low pass
filters 205, through the 495 .mu.m high pass reflector 208, through
the 527 nm high pass reflector 209, and through the lens 215 into
the reaction chamber 17. The excitation beam from LEDs 100C is thus
filtered to a wavelength below 495 nm corresponding to the peak
excitation range for FAM. When the green LEDs 100D are activated,
they generate an excitation beam that passes through the pair of
527 nm low pass filters 206, reflects off of the mirror 210,
reflects off of the 495 nm high pass reflector 208, passes through
the 527 nm high pass reflector 209, and passes through the lens 215
into the reaction chamber 17. The excitation beam from LEDs 100D is
thus filtered to a wavelength range of 495 to 527 nm corresponding
to the peak excitation range for TET. In operation, the LEDs 100A,
100B, 100C, 100D are sequentially activated to excite the different
fluorescent labels contained in the chamber 17 with excitation
beams in substantially distinct wavelength ranges.
[0134] FIG. 18 is a schematic, plan view of the optical detection
assembly 70. The assembly 70 is positioned adjacent the reaction
vessel 12 to receive light emitted from the chamber 17. FIG. 19 is
an exploded view of the detection assembly 70. As shown in FIGS.
18-19, the assembly 70 includes a housing 221 for holding various
components of the assembly.
[0135] The housing 221 includes the stops 247A, 247B previously
described with reference to FIGS. 13-14. The housing 221 preferably
comprises one or more molded plastic pieces. In the preferred
embodiment, the housing 221 is a multi-part housing comprised of
upper and lower housing elements 234A and 234B. The housing
elements 234A, 234B are complementary, mating pieces that are held
together by screws 214. In alternative embodiments, the entire
housing 221 may be a one-piece housing that holds a slide-in optics
package.
[0136] The lower housing element 234B includes an optical window
237 into which is placed a cylindrical rod lens 232 for collimating
light emitted from the chamber 17. In general, the optical window
may simply comprise an opening in the housing through which the
emitted light may be received. The optical window may optionally
include an optically transmissive or transparent piece of glass or
plastic serving as a window pane, or as in the preferred
embodiment, the lens 232 for collimating light emitted from the
chamber 17. The lens 232 preferably directly contacts one of the
optically transmissive side walls of the chamber 17.
[0137] The optics assembly 70 also includes four detectors 102A,
102B, 102C, and 102D for detecting light emitted from the chamber
17 that is received through the lens 232. In general, each detector
may be a photomultiplier tube, CCD, photodiode, or other known
detector. In the preferred embodiment, each detector is a PIN
photodiode. The detectors 102A, 102B, 102C, and 102D are preferably
rigidly fixed in recesses formed in the lower housing element 234B.
The detectors are electrically connected by leads 245 to the
optical circuit board 74 (see FIG. 8) which is preferably mounted
to the underside of the lower housing element 234B.
[0138] The optics assembly 70 further includes a set of filters and
lenses arranged in the housing 221 for separating light emitted
from the chamber 17 into different emission wavelength ranges and
for directing the light in each of the emission wavelength ranges
to a respective one of the detectors. As shown in FIG. 19, the
lower housing element 234B preferably includes walls 247 that
create separate detection channels in the housing, with one of the
detectors positioned at the end of each channel. The walls 247
preferably include slots for receiving and rigidly holding the
filters and lenses. The filters and lenses may also be rigidly
fixed in the housing 221 by an adhesive used alone, or more
preferably, with an adhesive used in combination with slots in the
housing.
[0139] Referring to FIG. 18, the filters in the optics assembly 70
may be selected to block light emitted from the chamber 17 outside
of any desired emission wavelength ranges. The optics assembly 70
may therefore be used with any fluorescent, phosphorescent,
chemiluminescent, or electrochemiluminescent labels of interest.
For purposes of illustration, one specific embodiment of the
assembly 70 will now be described in which the assembly is designed
to detect light emitted from the chamber 17 in the peak emission
wavelength ranges of FAM, TAMRA, TET, and ROX.
[0140] In this embodiment, the set of filters preferably includes a
515 nm Schott Glass.RTM. filter 222A positioned in front of the
first detector 102A, a 550 nm Schott Glass.TM. filter 222B
positioned in front of the second detector 102B, a 570 nm Schott
Glass.RTM. filter 222C positioned in front of the third detector
102C, and a 620 nm Schott Glass.RTM. filter 222D positioned in
front of the fourth detector 102D. These Schott Glass.RTM. filters
are commercially available from Schott Glass Technologies, Inc. of
Duryea, Pennsylvania. The optics assembly 70 also includes a pair
of 505 nm high pass filters 223 positioned in front of the first
detector 102A, a pair of 537 nm high pass filters 224 positioned in
front of the second detector 102B, a pair of 565 nm high pass
filters 225 positioned in front of the third detector 102C, and a
pair of 605 nm high pass filters 226 positioned in front of the
fourth detector 102D.
[0141] Although it is presently preferred to position a pair of
high pass filters in front of each detector for double filtering of
light, a single filter may be used in alternative embodiments. In
addition, a lens 242 is preferably positioned in each detection
channel between the pair of high pass filters and the Schott
Glass.RTM. filter for collimating the filtered light. The optics
assembly 70 further includes a 605 nm high pass reflector 227, a
mirror 228, a 565 nm low pass reflector 229, a 537 nm high pass
reflector 230, and a 505 nm high pass reflector 231. The reflecting
filters and mirrors 227-231 are preferably angularly offset by
30.degree. from the high pass filters 223-226. As shown in FIG. 19,
the detection assembly 70 also preferably includes a first aperture
238 positioned between each detector and Schott Glass.RTM. filter
222 and an aperture 240 positioned between each lens 242 and Schott
Glass.RTM. filter 222. The apertures 238, 240 reduce the amount of
stray or off-axis light that reaches the detectors 102A, 102B,
102C, and 102D.
[0142] Referring again to FIG. 18, the detection assembly 70
detects light emitted from the chamber 17 in four emission
wavelength ranges as follows. The emitted light passes through the
lens 232 and strikes the 565 nm low pass reflector 229. The portion
of the light having a wavelength in the range of about 505 to 537
nm (corresponding to the peak emission wavelength range of FAM)
reflects from the 565 nm low pass reflector 229, passes through the
537 nm high pass reflector 230, reflects from the 505 nm high pass
reflector 231, passes through the pair of 505 nm high pass filters
223, through the lens 242, through the 515 nm Schott Glass.RTM.
filter 222A, and is detected by the first detector 102A. Meanwhile,
the portion of the light having a wavelength in the range of about
537 to 565 nm (corresponding to the peak emission wavelength range
of TET) reflects from the 565 nm low pass reflector 229, reflects
from the 537 nm high pass reflector 230, passes through the pair of
537 nm high pass filters 224, through the lens 242, through the 550
nm Schott Glass.RTM. filter 222B, and is detected by the second
detector 102B.
[0143] Further, the portion of the light having a wavelength in the
range of about 565 to 605 nm (corresponding to the peak emission
wavelength range of TAMRA) passes through the 565 nm low pass
reflector 229, through the 605 nm high pass reflector 227, through
the pair of 565 nm high pass filters 225, through the lens 242,
through the 570 nm Schott Glass.RTM. filter 222C, and is detected
by the third detector 102C. The portion of the light having a
wavelength over 605 nm (corresponding to the peak emission
wavelength range of ROX) passes through the 565 nm low pass
reflector 229, reflects from the 605 nm high pass reflector 227,
reflects from the mirror 228, passes through the pair of 605 nm
high pass filters 226, through the lens 242, through the 620 nm
Schott Glass.RTM. filter 222D, and is detected by the fourth
detector 102D. In operation, the outputs of detectors 102A, 102B,
102C, and 102D are analyzed to determine the concentrations of each
of the different fluorescently-labeled analytes contained in the
chamber 17, as will be described in greater detail below.
[0144] FIG. 20 shows a multi-site reactor system 106 according to
the present invention. The reactor system 106 comprises a thermal
cycler 108 and a controller 112, such as a personal or network
computer. The thermal cycler 108 includes a base instrument 110 for
receiving multiple heat-exchanging modules 60 (previously described
with reference to FIG. 8). The base instrument 110 has a main logic
board with edge connectors 114 for establishing electrical
connections to the modules 60. The base instrument 110 also
preferably includes a fan 116 for cooling its electronic
components. The base instrument 110 may be connected to the
controller 112 using any suitable data connection, such as a
universal serial bus (USB), ethernet connection, or serial line. It
is presently preferred to use a USB that connects to the serial
port of controller 112. Alternatively, the controller may be built
into the base instrument 110.
[0145] The term "thermal cycling" is herein intended to mean at
least one change of temperature, i.e. increase or decrease of
temperature, in a reaction mixture. Therefore, samples undergoing
thermal cycling may shift from one temperature to another and then
stabilize at that temperature, transition to a second temperature
or return to the starting temperature. The temperature cycle may be
performed only once or may be repeated as many times as required to
study or complete the particular chemical reaction of interest. Due
to space limitations in patent drawings, the thermal cycler 108
shown in FIG. 20 includes only sixteen reaction sites provided by
the sixteen heat-exchanging modules 60 arranged in two rows of
eight modules each. It is to be understood, however, that the
thermal cycler can include any number of desired reaction sites,
i.e., it can be configured as a multi-hundred site instrument for
simultaneously processing hundreds of samples. Alternatively, it
may be configured as a small, hand held, battery-operated
instrument having, e.g., 1 to 4 reaction sites.
[0146] Each of the reaction sites in the thermal cycler 108 is
provided by a respective one of the heat-exchanging modules 60. The
modules 60 are preferably independently controllable so that
different chemical reactions can be run simultaneously in the
thermal cycler 108. The thermal cycler 108 is preferably modular so
that each heat-exchanging module 60 can be individually removed
from the base instrument 110 for servicing, repair, or replacement.
This modularity reduces downtime since all the modules 60 are not
off line to repair one, and the instrument 110 can be upgraded and
enlarged to add more modules as needed. The modularity of the
thermal cycler 108 also means that individual modules 60 can be
precisely calibrated, and module-specific schedules or corrections
can be included in the control programs, e.g., as a series of
module-specific calibration or adjustment charts.
[0147] In embodiments in which the base instrument 110 operates on
external power, e.g. 110 V AC, the instrument preferably includes
two power connections 122, 124. Power is received though the first
connection 122 and output through the second connection 124.
Similarly, the instrument 110 preferably includes network interface
inlet and outlet ports 118, 120 for receiving a data connection
through inlet port 118 and outputting data to another base
instrument through outlet port 120. As shown in the block diagram
of FIG. 21, this arrangement permits multiple thermal cyclers 108A,
108B, 108C, 108D to be daisy-chained from one controller 112 and
one external power source 128.
[0148] FIG. 22 is a schematic, block diagram of the base instrument
110. The base instrument includes a power supply 134 for supplying
power to the instrument and to each module 60. The power supply 134
may comprise an AC/DC converter for receiving power from an
external source and converting it to direct current, e.g., for
receiving 110V AC and converting it to 12V DC. Alternatively, the
power supply 134 may comprise a battery, e.g., a 12V battery. The
base instrument 110 also includes a microprocessor or
microcontroller 130 containing firmware for controlling the
operation of the base instrument 110 and modules 60. The
microcontroller 130 communicates through a network interface 132 to
the controller computer via a USB. Due to current limitations of
processing power, it is currently preferred to include at least one
microcontroller in the base instrument per sixteen modules 60. Thus
if the base instrument has a thirty-two module capacity, at least
two microcontrollers should be installed in the instrument 110 to
control the modules.
[0149] The base instrument 110 further includes a heater power
source and control circuit 136, a power distributor 138, a data bus
140, and a module selection control circuit 142. Due to space
limitations in patent drawings, control circuit 136, power
distributor 138, data bus 140, and control circuit 142 are shown
only once in the block diagram of FIG. 22. However, the base
instrument 110 actually contains one set of these four functional
components 136, 138, 140, 142 for each heat-exchanging module 60.
Thus, in the embodiment of FIG. 22, the base instrument 110
includes sixteen control circuits 136, power distributors 138, data
buses 140, and control circuits 142. Similarly, the base instrument
110 also includes a different edge connector 131 for connecting to
each of the modules 60, so that the instrument includes sixteen
edge connectors for the embodiment shown in FIG. 22. The edge
connectors are preferably 120 pin card edge connectors that provide
cableless connection from the base instrument 110 to each of the
modules 60. Each control circuit 136, power distributor 138, data
bus 140, and control circuit 142 is connected to a respective one
of the edge connectors and to the microcontroller 130.
[0150] Each heater power and source control circuit 136 is a power
regulator for regulating the amount of power supplied to the
heating element(s) of a respective one of the modules 60. The
source control circuit 136 is preferably a DC/DC converter that
receives a +12V input from the power supply 134 and outputs a
variable voltage between 0 and -24V. The voltage is varied in
accordance with signals received from the microcontroller 130. Each
power distributor 138 provides -5V, +5V, +12V, and GND to a
respective module 60. The power distributor thus supplies power for
the electronic components of the module. Each data bus 140 provides
parallel and serial connections between the microcontroller 130 and
the digital devices of a respective one of the modules 60. Each
module selection controller 94 allows the microcontroller 130 to
address an individual module 60 in order to read or write control
or status information.
[0151] FIG. 23 is a schematic, block diagram of the electronic
components of a heat-exchanging module 60. Each module includes an
edge connector 80 for cableless connection to a corresponding edge
connector of the base instrument. The module also includes heater
plates 50A, 50B each having a resistive heating element as
described above. The plates 50A, 50B are wired in parallel to
receive power input 146 from the base instrument. The plates 50A,
50B also include temperature sensors 52, e.g. thermistors, that
output analog temperature signals to an analog-to-digital converter
154. The converter 154 converts the analog signals to digital
signals and routes them to the microcontroller in the base
instrument through the edge connector 80. The heat-exchanging
module also includes a cooling system, such as a fan 66, for
cooling the plates 50A, 50B. The fan 66 receives power from the
base instrument and is activated by switching a power switch 164.
The power switch 164 is in turn controlled by a control logic block
162 that receives control signals from the microcontroller in the
base instrument.
[0152] The module further includes four light sources, such as LEDs
100, for excitation of labeled analytes in the reaction mixture and
four detectors 102, preferably photodiodes, for detecting
fluorescent emissions from the reaction mixture. The module also
includes an adjustable current source 150 for supplying a variable
amount of current (e.g., in the range of 0 to 30 mA) to each LED to
vary the brightness of the LED. A digital-to-analog converter 152
is connected between the adjustable current source 150 and the
microcontroller of the base instrument to permit the
microcontroller to adjust the current source digitally. The
adjustable current source 150 may be used to ensure that each LED
has about the same brightness when activated. Due to manufacturing
variances, many LEDs have different brightnesses when provided with
the same amount of current. The brightness of each LED may be
tested during manufacture of the heat-exchanging module and
calibration data stored in a memory 160 of the module. The
calibration data indicates the correct amount of current to provide
to each LED. The microcontroller reads the calibration data from
the memory 160 and controls the current source 150 accordingly. The
microcontroller may also control the current source 150 to adjust
the brightness of the LEDs 100 in response to optical feedback
received from the detectors 102.
[0153] The module additionally includes a signal conditioning/gain
select/offset adjust block 156 comprised of amplifiers, switches,
electronic filters, and a digital-to-analog converter. The block
156 adjusts the signals from the detectors 102 to increase gain,
offset, and reduce noise. The microcontroller in the base
instrument controls block 156 through a digital output register
158. The output register 158 receives data from the microcontroller
and outputs control voltages to the block 156. The block 156
outputs the adjusted detector signals to the microcontroller
through the analog-to-digital converter 154 and the edge connector
80. The module also includes the memory 160, preferably a serial
EEPROM, for storing data specific to the module, such as
calibration data for the LEDs 100, thermal plates 50A, 50B, and
temperature sensors 52, as well as calibration data for a
deconvolution algorithm described in detail below.
[0154] Referring again to FIG. 20, the reactor system 106 may be
configured for manual filling and pressurization of each reaction
vessel 12 by a human operator. Manual use of the system is suitable
for lower throughput embodiments. For higher throughput
embodiments, however, the system 106 preferably includes automated
machinery, e.g., a pick-and-place machine, for filling and
pressurizing each of the vessels 12.
[0155] FIG. 24 shows a schematic diagram of a pick-and-place
machine 166 for automatically filling and pressurizing a reaction
vessel 12. The machine 166 has a pipette head 168 for engaging a
disposable pipette tip 170. The machine 166 also has controllable
vacuum and pressure sources in communication with the pipette head
168 for aspirating and dispensing fluids using the pipette tip 170.
The vacuum and pressure sources may comprise, e.g., one or more
syringe pumps, compressed air sources, pneumatic pumps, vacuum
pumps, or connections to external sources of pressure.
[0156] As shown in FIG. 25, the pick-and-place machine 166 also has
a robotic arm or machine tip 172 for picking and placing the
plunger 22 into the channel 28 of the reaction vessel 12. The
machine tip 172 may optionally include an alignment pin 174 for
aligning the cap 36 of the plunger in a desired angular orientation
with respect to the body of the vessel 12. The alignment pin 174
provides a convenient mechanism for rotating the cap to the desired
orientation before inserting the plunger 22 into the channel 28. As
previously shown in FIG. 3, the cap 36 includes a tapered
engagement aperture 46 for receiving and establishing a friction
fit with the machine tip. The cap 36 also includes alignment
apertures 48A, 48B, either one of which may receive the alignment
pin. Referring again to FIG. 25, the pick-and-place machine 166
also preferably includes an ejector plate 176 that slides down the
machine tip 172 to eject the plunger 22 from the machine tip after
the plunger is inserted into the channel 28. Although this
embodiment of the pick-and-place machine is presently preferred,
many other embodiments are possible. For example, the machine tip
172 may be designed to establish a vacuum fit with the cap 36 of
the plunger. Alternatively, the pick-and-place machine may have a
robotic gripper arm for gripping the plunger 22 and inserting it
into the channel 28. Suitable pick-and-place machines for use in
the apparatus of the present invention are commercially available
as machines built to specification from several suppliers, such as
Tecan U.S. Inc. located at 4022 Stirrup Creek Drive, Durham, N.C.
27703.
[0157] Referring again to FIG. 20, the controller 112 preferably
includes software for controlling the thermal cycler 108 and the
pick-and-place machine (described above with reference to FIGS.
24-25) to perform the functions described in the operation section
below. These functions include providing a user interface to enable
a user to select desired thermal processing parameters (e.g., set
point temperatures and hold times at each temperature) and optical
detection parameters, automatic filling and pressurization of the
vessels 12, thermal processing of the vessels according to the
selected parameters, optical interrogation of the reaction mixtures
in the vessels, and recording of the optical data generated. The
creation of software and/or firmware for performing these functions
can be performed by a computer programmer having ordinary skill in
the art. Moreover, the software and/or firmware may reside solely
in the controller 112 or may be distributed between the controller
and one or more microprocessors in the thermal cycler or
pick-and-place machine. Alternatively, the controller 112 may
simply be built into the thermal cycler or pick-and-place
machine.
[0158] In operation, the reactor system 106 is used to thermally
process and optically interrogate one or more samples. An exemplary
use of the system 106 is for the amplification of nucleic acid in a
sample (e.g., using PCR) and for the optical detection of one or
more target analytes in the sample. A user selects a desired
thermal profile for the sample using, e.g., the keyboard or mouse
of the controller 112. For example, for a PCR amplification, the
user may select the thermal profile to begin with a 30 second
induction hold at 95.degree. C., followed by 45 thermal cycles in
which the reaction mixture is cycled between higher and lower
temperatures for denaturization, annealing, and polymerization. For
example, each thermal cycle may include a first set point
temperature of 95.degree. C. which is held for 1 second to denature
double-stranded DNA, followed by a second set point temperature of
60.degree. C. which is held for 6 seconds for annealing of primers
and polymerization.
[0159] Referring again to FIG. 24, the sample is preferably
dispensed into the vessel 12 by aspirating the sample into the
pipette tip 170, inserting the pipette tip 170 through the channel
28 into the chamber 17, and dispensing the sample into the chamber.
It is presently preferred that the chamber 17 be filled from the
bottom up by initially inserting the pipette tip 170 close to the
bottom of the chamber 17 and by slowly retracting the pipette tip
170 as the chamber 17 is filled. Filling the chamber 17 in this
manner reduces the likelihood that air bubbles will form in the
chamber. Such air bubbles could have a negative effect on
subsequent optical detection.
[0160] The fluid sample may be mixed with chemicals necessary for
the intended reaction (e.g., PCR reagents and/or fluorescent
probes) prior to being added to the chamber 17. Alternatively, the
sample may be introduced to the chemicals in the chamber 17, e.g.,
by adding the chemicals to the chamber before or after the sample
to form the desired reaction mixture in the chamber. In a
particularly advantageous embodiment, the necessary reagents and/or
fluorescent probes for the intended reaction are placed in the
chamber 17 when the vessel is manufactured. The reagents are
preferably placed in the chamber 17 in dried or lyophilized form so
that they are adequately preserved until the vessel is used.
[0161] Referring again to FIG. 25, the chamber 17 is then
pressurized after it is filled with the reaction mixture. To
increase pressure in the vessel, the machine tip 172 of the
pick-and-place machine 166 engages the cap 36 of the plunger 22 and
inserts the plunger into the channel 28 until the snap ring 38
snaps into the annular recess 23. As the plunger 22 is inserted,
the piston 32 compresses gas in the channel 28 to increase pressure
in the chamber 17, preferably to about 8 to 15 psi above ambient
pressure, as previously discussed with reference to FIGS. 7A-7D.
After the plunger 22 is inserted, the ejector plate 176 ejects the
plunger 22 from the machine tip 172.
[0162] Referring again to FIG. 20, each of the vessels 12 may be
inserted between the thermal plates of a respective heat-exchanging
module 60 either prior to filling and pressurizing the vessel or
after filling and pressurizing the vessel. In either case, as shown
in FIG. 5, the pressure in the chamber 17 forces the flexible major
walls 18 to contact and conform to the inner surfaces of the plates
50. In embodiments in which the vessels are inserted between the
plates prior to filling and pressurization, the pick-and-place
machine includes a robotic arm (not shown) for picking up the
vessels and inserting them into the modules. Robotic arms for
picking and placing reaction vessels are well known in the art.
[0163] Referring again to FIG. 25, each vessel 12 may alternatively
be inserted between the plates of a respective module after filling
and pressurization using the machine tip 172. In this embodiment,
the vessel 12 is preferably held in a rack, tray, or similar
support device during filling and pressurization. After the vessel
12 is filled and pressurized, the machine tip 172 picks up the
vessel 12 by the cap 36 of the plunger 22 and inserts the chamber
17 of the vessel between the plates of a heat-exchanging module.
The plunger 22 is held in the channel 28 during this movement by
the snap ring 38 that engages the annular recess 23. After the
vessel 12 is inserted, the ejector plate 176 ejects the cap 36 from
the machine tip 172.
[0164] Although automated filling and pressurization of the vessel
12 has been described, the vessel may also be manually filled and
pressurized by a human operator. This is most easily accomplished
by filling the chamber 17 using a hand-held pipette or syringe and
by manually inserting the plunger 22 into the channel 28. The
operator then inserts the chamber 17 of the vessel into one of the
heat-exchanging modules.
[0165] Referring again to FIG. 20, once a filled and pressurized
reaction vessel 12 is placed between the thermal plates of a
heat-exchanging module 60, the reaction mixture contained in the
vessel is subjected to the thermal profile selected by the user.
The controller 112 preferably implements standard
proportional-integral-derivative (PID) control to execute the
selected thermal profile. Referring again to FIG. 23, the
controller receives signals indicating the temperatures of the
plates 50A, 50B from the temperature sensors 52. Polling of the
plate temperatures preferably occurs every 100 milliseconds
throughout the running of the temperature profile. After each
polling, the controller averages the temperatures of the two plates
50A, 50B to determine an average plate temperature. The controller
then determines the difference (delta) between the profile target
temperature, i.e. the set point temperature defined by the user for
the particular time in the profile, and the average plate
temperature. Based on the relationship between the average plate
temperature and the current target temperature, the controller
controls the amount of power supplied to the heating elements on
the plates 50A, 50B or to the fan 66 as appropriate to reach or
maintain the current set point temperature. Standard PID control is
well known in the art and need not be described further herein.
[0166] The controller may optionally implement a modified version
of PID control described in International Publication Number WO
99/48608 published Sep. 30, 1999, the disclosure of which is
incorporated by reference herein. In this modified version of PID
control, the controller is programmed to compensate for thermal lag
between the plates 50A, 50B and a reaction mixture contained in a
reaction vessel inserted between the plates. The thermal lag is
caused by the need for heat to transfer from the plates 50A, 50B
through the flexible walls of the vessel and into the reaction
mixture during heating, or by the need for heat to transfer from
the reaction mixture through the walls of the vessel to the plates
50A, 50B during cooling. In standard PID control, the power
supplied to a heating or cooling element is dependent upon the
difference (error) between the actual measured temperature of the
plates and the desired set point temperature. The average power
being supplied to either the heating or cooling element therefore
decreases as the actual temperature of the plates approaches the
set point temperature, so that the reaction mixture does not reach
the set point temperature as rapidly as possible. The modified
version of PID control overcomes this disadvantage of standard PID
control during rapid heating or cooling steps.
[0167] To compensate for the thermal lag during heating steps
(i.e., to raise the temperature of the reaction mixture to a
desired set point temperature that is higher than the previous set
point temperature), the controller sets a variable target
temperature that initially exceeds the desired set point
temperature. For example, if the set point temperature is
95.degree. C., the initial value of the variable target temperature
may be set 2 to 10.degree. C. higher. The controller next
determines a level of power to be supplied to the heating elements
to raise the temperature of the plates 50A, 50B to the variable
target temperature by inputting the variable target temperature and
the current average plate temperature to a standard PID control
algorithm. The level of power to be supplied to the heaters is
therefore determined in dependence upon the difference (error)
between the average plate temperature and a target temperature that
is higher than the desired set point temperature. The higher target
temperature ensures that a higher level of power is supplied to
heat the plates 50A, 50B, and therefore the reaction mixture, to
the set point temperature more rapidly. The controller then sends a
control signal to the power and source control circuit in the base
instrument to provide power to the heating elements at the level
determined.
[0168] When the temperature of the plates 50A, 50B is subsequently
polled, the controller determines if the actual measured
temperature of the plates is greater than or equal to a
predetermined threshold value. Suitable threshold values are: the
desired set point temperature itself; or 1 to 2.degree. C. below
the set point temperature, e.g., 93 to 94.degree. C. for a set
point temperature of 95.degree. C. If the average plate temperature
does not exceed the predetermined threshold value, then the
controller again determines a level of power to be supplied to the
heating elements in dependence upon the difference between the
average plate temperature and the target temperature and sends
another control signal to provide power to the heaters at the level
determined. This process is repeated until the average plate
temperature is greater than or equal to the threshold value.
[0169] When the average plate temperature is greater than or equal
to the threshold value, the controller decreases the variable
target temperature, preferably by exponentially decaying the amount
by which the variable target temperature exceeds the set point
temperature. For example, the amount by which the variable target
temperature exceeds the desired set point temperature may be
exponentially decayed as a function of time according to the
equation:
.DELTA.=(.DELTA..sub.max)*e.sup.(-t/tau)
where .DELTA. is equal to the amount by which the variable target
temperature exceeds the desired set point temperature,
.DELTA..sub.max is equal to the difference between the initial
value of the variable target temperature and the desired set point
temperature, t is equal to the elapsed time in seconds from the
start of decay, and tau is equal to a decay time constant.
[0170] In the system of the present invention, tau preferably has a
value in the range of 1 to 4 seconds. It is presently preferred to
determine tau empirically for the heat-exchanging module during
testing and calibration of the module and to store the value of tau
in the memory 160 of the module before shipping it to the end user.
Although the exponential equation given above is presently
preferred, it is to be understood that many other decay formulas
may be employed and fall within the scope of the invention.
Moreover, the variable target temperature may be decreased by other
techniques, e.g., it may be decreased linearly.
[0171] After decreasing the variable target temperature, the
controller determines a new level of power to be supplied to the
heating elements to raise the temperature of the plates 50A, 50B to
the decreased target temperature. The controller determines the
level of power by inputting the current plate temperature and
decreased target temperature to the PID control algorithm. The
controller then sends a control signal to provide power to the
heaters at the new level determined. As the time in the thermal
profile progresses, the controller continues to decrease the
variable target temperature until it is equal to the set point
temperature. When the variable target temperature is equal to the
set point temperature, standard PID control is resumed to maintain
the plates 50A, 50B at the set point temperature.
[0172] To compensate for the thermal lag during cooling steps
(i.e., to lower the temperature of the reaction mixture to a
desired set point temperature that is lower than the previous set
point temperature), the controller preferably activates the fan 66
just prior to the completion of the previous set point temperature
to allow the fan to achieve maximum speed for cooling (i.e., to
allow for spin-up time). The controller then sets a variable target
temperature that is initially lower than the desired set point
temperature. For example, if the set point temperature is
60.degree. C., the initial value of the variable target temperature
may be set 2 to 10.degree. C. lower, i.e., 50 to 58.degree. C. The
controller continues cooling with the fan 66 until the actual
measured temperature of the plates 50A, 50B is less than or equal
to a threshold value, preferably the variable target temperature.
When the average plate temperature is less than or equal to the
variable target temperature, the controller deactivates the fan 66
and increases the target temperature, preferably by exponentially
decaying the amount by which the variable target temperature
differs from the set point temperature using the exponential decay
equation given above. For cooling, tau is preferably in the range
of 1 to 5 seconds with a preferred value of about 3 seconds. As in
the heating example given above, tau may be determined empirically
for the heat-exchanging module during testing or calibration and
stored in the memory 160.
[0173] The controller next determines a level of power to be
supplied to the heating elements to raise the temperature of the
plates 50A, 50B to the increased target temperature by inputting
the current average plate temperature and the increased target
temperature to the PID control algorithm. The controller then sends
a control signal to the power and source control circuit in the
base instrument to provide power to the heating elements at the
level determined. As time in the thermal profile continues, the
controller continues to increase the variable target temperature
and issue control signals in this manner until the variable target
temperature is equal to the set point temperature. When the
variable target temperature is equal to the set point temperature,
the controller resumes standard PID control to maintain the plates
50A, 50B at the set point temperature.
[0174] Referring again to FIGS. 16 and 18, the reaction mixture in
the vessel 12 is optically interrogated in real-time as the thermal
profile is executed to determine if the mixture contains one or
more target analytes. In the preferred embodiment, the mixture is
optically interrogated once per thermal cycle at the lowest
temperature in the cycle. Optical interrogation is accomplished by
sequentially activating LEDs 100A, 100B, 100C, and 100D to excite
different fluorescently-labeled analytes in the mixture and by
detecting light emitted (fluorescent output) from the chamber 17
using detectors 102A, 102B, 102C, and 102D. In the following
example of operation, the fluorescent dyes FAM, TAMRA, TET, and ROX
are used to label the target analytes, e.g., target nucleotide
sequences, nucleic acids, proteins, pathogens, or organisms in the
reaction mixture.
[0175] There are four pairs of LEDs 100A, 100B, 100C, and 100D and
four detectors 102A, 102B, 102C, and 102D for a total of sixteen
combinations of LED/detector pairs. It is theoretically possible to
collect output signals from the detectors for all sixteen
combinations. Of these sixteen combinations, however, there are
only four primary detection channels. Each primary detection
channel is formed by a pair of LEDs in the optics assembly 68 whose
excitation beams lie in the peak excitation wavelength range of a
particular dye and by one corresponding detection channel in the
optics assembly 70 designed to detect light emitted in the peak
emission wavelength range of the same dye. The first primary
detection channel is formed by the first pair of LEDs 100A and the
fourth detector 102D (the ROX channel). The second primary
detection channel is formed by the second pair of LEDs 100B and the
third detector 102C (the TAMRA channel). The third primary
detection channel is formed by the third pair of LEDs 100C and the
first detector 102A (the FAM channel). The fourth primary detection
channel is formed by the fourth pair of LEDs 100D and the second
detector 102B (the TET channel).
[0176] Prior to activating any of the LEDs 100A, 100B, 100C, 100D,
a "dark reading" is taken to determine the output signal of each of
the four detectors 102A, 102B, 102C, 102D when none of the LEDs are
lit. The "dark reading" signal output by each detector is
subsequently subtracted from the corresponding "light reading"
signal output by the detector to correct for any electronic offset
in the optical detection circuit. This procedure of obtaining "dark
reading" signals and subtracting the dark signals from the
corresponding "light reading" signals is preferably performed every
time that a reaction vessel is optically interrogated, including
those times the vessel is interrogated during the development of
calibration data (described in detail below). For clarity and
brevity of explanation, however, the steps of obtaining "dark
reading" signals and subtracting the dark signals from the
corresponding "light reading" signals will not be further repeated
in this description.
[0177] Following the dark reading, a "light reading" is taken in
each of the four primary optical detection channels as follows. The
first pair of LEDs 100A is activated and the LEDs generate an
excitation beam that passes through the pair of 593 nm low pass
filters 203, reflects off of the 593 nm low pass reflector 212,
passes through the 555 nm low pass reflector 211, reflects off of
the 527 nm high pass reflector 209, and passes through the lens 215
into the reaction chamber 17. The excitation beam from the LEDs
100A is thus filtered to a wavelength range of 555 to 593 nm
corresponding to the peak excitation range for ROX. As shown in
FIG. 18, emitted light (fluorescence emission radiation) from the
chamber 17 passes through the lens 232 of the detection assembly 70
and strikes the 565 nm low pass reflector 229. The portion of the
light having a wavelength over 605 nm (corresponding to the peak
emission wavelength range of ROX) passes through the 565 nm low
pass reflector 229, reflects from the 605 nm high pass reflector
227, reflects from the mirror 228, passes through the pair of 605
nm high pass filters 226, through the lens 242, through the 620 nm
Schott Glass.RTM. filter 222D, and is detected by the fourth
detector 102D. The fourth detector 102D outputs a corresponding
signal that is converted to a digital value and recorded.
[0178] Next, as shown in FIG. 16, the second pair of LEDs 100B is
activated and the LEDs generate an excitation beam that passes
through the pair of 555 nm low pass filters 204, reflects off of
the 555 nm low pass reflector 211, reflects off of the 527 nm high
pass reflector 209, and passes through the lens 215 into the
reaction chamber 17. The excitation beam from LEDs 100B is thus
filtered to a wavelength range of 527 to 555 nm corresponding to
the peak excitation range for TAMRA. As shown in FIG. 18, emitted
light from the chamber 17 then passes through the lens 232 of the
detection assembly 70 and strikes the 565 nm low pass reflector
229. The portion of the light having a wavelength in the range of
about 565 to 605 nm (corresponding to the peak emission wavelength
range of TAMRA) passes through the 565 nm low pass reflector 229,
through the 605 nm high pass reflector 227, through the pair of 565
nm high pass filters 225, through the lens 242, through the 570 nm
Schott Glass.RTM. filter 222C, and is detected by the third
detector 102C. The third detector 102C outputs a corresponding
signal that is converted to a digital value and recorded.
[0179] Next, as shown in FIG. 16, the pair of blue LEDs 100C is
activated and the LEDs generate an excitation beam that passes
through the pair of 495 nm low pass filters 205, through the 495 nm
high pass reflector 208, through the 527 nm high pass reflector
209, and through the lens 215 into the reaction chamber 17. The
excitation beam from LEDs 100C is thus filtered to a wavelength
range of about 450 to 495 nm corresponding to the peak excitation
range for FAM. As shown in FIG. 18, emitted light from the chamber
17 then passes through the lens 232 of the detection assembly 70
and strikes the 565 nm low pass reflector 229. The portion of the
light having a wavelength in the range of about 505 to 537 nm
(corresponding to the peak emission wavelength range of FAM)
reflects from the 565 nm low pass reflector 229, passes through the
537 nm high pass reflector 230, reflects from the 505 nm high pass
reflector 231, passes through the pair of 505 nm high pass filters
223, through the lens 242, through the 515 nm Schott Glass.RTM.
filter 222A, and is detected by the first detector 102A. The first
detector 102A outputs a corresponding signal that is converted to a
digital value and recorded.
[0180] Next, as shown in FIG. 16, the fourth pair of LEDs 100D is
activated and the LEDs generate an excitation beam that passes
through the pair of 527 nm low pass filters 206, reflects off of
the mirror 210, reflects off of the 495 nm high pass reflector 208,
passes through the 527 nm high pass reflector 209, and passes
through the lens 215 into the reaction chamber 17. The excitation
beam from LEDs 100D is thus filtered to a wavelength range of 495
to 527 nm corresponding to the peak excitation range for TET. As
shown in FIG. 18, emitted light from the chamber 17 then passes
through the lens 232 of the detection assembly 70 and strikes the
565 nm low pass reflector 229. The portion of the light having a
wavelength in the range of about 537 to 565 nm (corresponding to
the peak emission wavelength range of TET) reflects from the 565 nm
low pass reflector 229, reflects from the 537 nm high pass
reflector 230, passes through the pair of 537 nm high pass filters
224, through the lens 242, through the 550 nm Schott Glass.RTM.
filter 222B, and is detected by the second detector 102B. The
second detector 102B outputs a corresponding signal that is
converted to a digital value and recorded. The total time required
to activate each of the four LEDs 100A, 100B, 100C, 100D in
sequence and to collect four corresponding measurements from the
detectors 102A, 102B, 102C, 102D is typically five seconds or
less.
[0181] The spectrum of the fluorescence that is emitted by the dyes
used for detection is usually broad. As a result, when an
individual dye (e.g., FAM, TAMRA, TET, or ROX) emits fluorescence
from the reaction vessel 12, the fluorescence can be detected in
several of the primary detection channels, i.e. several of the
detectors 102A, 102B, 102C, and 102D detect the fluorescence and
generate an output signal. However, each dye has its own
`signature`, i.e., the ratios of the optical signals in each
detection channel are unique to each dye. It is also a reasonable
assumption that the fluorescent emission from a mixture of dyes are
simply additive in each of the detection channels, so that the
individual dye concentrations of a dye mixture can be extracted
from the mixed signals using linear algebra.
[0182] In the preferred embodiment, the controller is programmed to
convert the output signals of the detectors to values indicating
the true concentration of each dye labeling a respective analyte in
the reaction mixture using linear algebra and a calibration matrix.
A preferred method for developing the calibration matrix will now
be described using the four-channel optical system of the preferred
embodiment as an example. First, a reaction vessel containing only
reaction buffer is optically read using optics assemblies 68, 70.
The reaction buffer should be a fluid similar or nearly identical
to the reaction mixtures that will be optically read by the optics
assemblies during actual production use of the system to test
samples. The reaction buffer should contain no dyes, so that the
concentrations of all dyes are zero. The optical reading of the
reaction buffer in the four primary detection channels produces
four output signals that are converted to corresponding digital
values. These four numbers are called Buffer(I), where `I` is 1, 2,
3 or 4 depending upon which detection channel is read. The buffer
values are a measure of the background signal or scattered light
detected in each primary detection channel without any added
fluorescent signal from dyes.
[0183] Next, a reaction mixture containing a known concentration,
e.g. 100 nM, of dye # 1 is placed into the vessel and again the
four channels are read. The four numbers produced are called
Rawdye(I, 1). Similar sets of four numbers are obtained for the
other three dyes to obtain Rawdye(I, 2), Rawdye(I, 3), and
Rawdye(I, 4). The buffer values are then subtracted from the raw
dye values to obtain net dye values as follows:
Netdye(I,J)=Rawdye(I,J)-Buffer(I);
where I indicates the detection channel, and J indicates the dye
number.
[0184] The matrix Netdye(I, J) is then inverted using standard
numerical methods (such as Gaussian elimination) to obtain a new
matrix called the calibration matrix Cal(I,J). Note that the matrix
product of Netdye(I, J)*Cal (I,J) is the unity matrix. Now, any
reaction mixture can be read and the output signals of the
detectors in the four detection channels converted to values
representative of the true concentrations of dyes labeling analytes
in the mixture. The optical reading of the mixture produces four
numbers called RawMix(I). The reaction buffer values are then
subtracted from the raw mix values to obtain four numbers called
Mix(I) as follows:
Mix(I)=RawMix(I)-Buffer(I)
[0185] Next, the true concentrations of the dyes labeling analytes
are obtained by matrix multiplication as follows:
Truedye(I)=100 nM*Cal(I,J)*Mix(I)
[0186] In the above equation, the factor of 100 comes from the fact
that a concentration of 100 nM was used for the initial calibration
measurements. The concentration of 100 nM is used for purposes of
example only and is not intended to limit the scope of the
invention.
[0187] In general, the dye concentrations for calibration
measurements should be somewhere in the range of 25 to 1,000 mM
depending upon the fluorescent efficiency (strength) of the dyes
and their use in a particular assay or application.
[0188] Referring again to FIGS. 22-23, the matrices Cal(I, J) and
Buffer(I) are preferably produced during the manufacture of each
heat-exchanging module 60 and stored in the memory 160. When the
module 60 is plugged into the base instrument 110, the control
software application in the base instrument or external computer
reads the matrices into memory and uses the matrices to convert the
output signals of the detectors 102 to values indicating the
concentration of each dye in the reaction mixture. Because the
calibration matrices Cal(I, J) and Buffer(I) are dependent upon the
particular set of dyes calibrated and the volume of the reaction
vessel, it is also preferred to produce and store multiple sets of
the matrices for various combinations of dye sets and reaction
vessel volumes. This gives the end user greater flexibility in
using the system.
[0189] As one example, calibration matrices could be stored for
three different dyo sets to be used with three different sizes of
reaction vessels (e.g., 25 .mu.l, 50 .mu.l, 100 .mu.l) for a total
of nine different sets of calibration matrices. Of course, this is
just one example, and many other combinations will be apparent to
one skilled in the art upon reading this description. Further, in
alternative embodiments, the control software may include
functionality to guide the end user through the calibration
procedure to enable the user to store and use calibration data for
his or her own desired combination of dyes and reaction vessel
size.
[0190] It is presently preferred to perform an optical reading of
the reaction mixture once per thermal cycle at the lowest
temperature in the cycle. Alternatively, the reaction mixture could
be optically monitored more frequently or less frequently as
desired by the user. One advantage to frequent optical monitoring
is that real-time optical data may be used to indicate the progress
of the reaction. For example, when a particular predetermined
fluorescent threshold is detected in a reaction mixture in a
heat-exchanging module, then the temperature cycling for that
module may be stopped. Furthermore, optical detection of dye
activation, e.g., color change, is useful to control the cycle
parameters, not only thermal schedules, but also the state or
condition of reactants and products, and quantitative production.
Multiple emission wavelengths can be sampled to determine, for
example, progression of the reaction, end points, triggers for
reagent addition, denaturization (melting), annealing and the like.
The data obtained in the real-time monitoring method may be fed
back to the controller to alter or adjust the optical "read"
parameters. Examples of the optical read parameters include: length
of read; power input or frequency to the LEDs; which wavelength
should be monitored and when; and the like.
[0191] In a typical implementation of the four-channel system,
three of the optical channels are used to detect target analytes
(e.g., amplified nucleic acid sequences) while the fourth channel
is used to monitor an internal control to check the performance of
the system. For example, beta actin is often used as an internal
control in nucleic acid amplification reactions because it has a
predictable amplification response and can be easily labeled and
monitored to verify that the amplification is occurring
properly.
[0192] One advantage of the apparatus of the preferred embodiment
is that it provides extremely rapid heating and cooling of a
reaction mixture. This rapid heating and cooling is particularly
beneficial for nucleic acid amplification because of the increased
speed with which the amplification may be accomplished and because
it significantly reduces the likelihood of creating unwanted and
interfering side products, such as PCR "primer-dimers" or anomalous
amplicons. Another advantage of the apparatus is that it provides
for sensitive, real-time detection of one or more analytes in a
reaction mixture as the reaction is performed. In experimental
testing of the apparatus of the preferred embodiment, extraordinary
results for nucleic acid amplification and detection were achieved.
For example, a 100 .mu.l sample containing bacillus globigii in a
starting concentration of 105 copies per ml has been amplified and
detected in about 8 minutes (24 thermal cycles having a duration of
21 seconds per cycle).
[0193] FIG. 26 shows a reaction vessel 180 according to another
embodiment of the invention. The vessel 180 is similar to the
vessel of the preferred embodiment (described with reference to
FIGS. 1-2), except that the vessel 180 has a smaller reaction
chamber 184. The size of the chamber 184 is defined by the side
walls 186A, 186B, 188A, 188B and by the thickness of the rigid
frame 182. In this embodiment, each of the side walls 186A, 186B,
188A, 188B has a length L of about 5 mm, the chamber has a width W
of about 7 mm, and the chamber has a thickness T of 1 mm so that
the chamber has a volume capacity of 25 .mu.L. The advantage to the
vessel 180 is that it holds a smaller volume of reaction mixture so
that the mixture requires less reagent. The disadvantage is that
the smaller volume may cause decreased sensitivity in the detection
of low concentration analytes, such as nucleic acids. The vessel
180 demonstrates that the reaction vessels of the present invention
may be fabricated with chambers having various volume capacities,
preferably in the range of 5 to 200 .mu.l. It is presently
preferred to fabricate each of the vessels with substantially the
same size frame, regardless of the volume capacity of the chamber,
so that each of the vessels may be used with the same size
heat-exchanging module 60 (FIG. 8).
[0194] FIG. 27 shows a reaction vessel 190 according to another
embodiment of the invention. The vessel 190 is similar to the
vessel of the preferred embodiment (described with reference to
FIGS. 1-2), except that the vessel 190 has an elastomeric plunger
192. The plunger 192 is constructed of an elastomeric material,
e.g., a thermal plastic elastomer (TPE) or silicone. The
elastomeric plunger 192 preferably includes a sealing ring 194 that
establishes a seal with the walls of the channel 193 when the
plunger is inserted into the channel to compress gas in the vessel
and increase pressure in the chamber 191. The plunger 192 may be
manually inserted into the channel 193 by human hands, or
alternatively, the plunger 192 may include an engagement aperture
to permit a pick-and-place machine to pick and place the plunger
into the channel.
[0195] FIG. 28 shows a reaction vessel 250 according to another
embodiment of the invention. The vessel 250 is similar to the
vessel of the preferred embodiment (described with reference to
FIGS. 1-2), except that the vessel 250 has several additional
features. In particular, the plunger 252 of the vessel has a
plunger cap 259 on which are formed ramp-shaped protrusions 260A,
260B. The vessel includes corresponding ramp-shaped protrusions
262A, 262B which are preferably formed on the finger grips 26 and
positioned on opposite sides of the port 14. The corresponding sets
of ramp-shaped protrusions engage each other provide for easy
twist-off of the plunger 252, if desired, after the vessel 250 is
used.
[0196] The plunger 252 also includes a stem 254 that terminates in
a tongue 258. As shown in FIG. 29, the stem 254 has a length
substantially equal to the length of the channel 28 so that the tip
of the tongue 258 is positioned at the end of the channel 28
adjacent the entrance 266 to the chamber 17 when the plunger 252 is
fully inserted in the channel. The advantage of the tongue 258 is
that it provides a physical barrier for preventing the reaction
mixture in the chamber 17 from bubbling up (refluxing) or
evaporating into the channel 28 as the mixture is heated. As shown
in FIG. 30, the cap 259 may also include an engagement aperture 46
and alignment apertures 48A, 48B to permit automated picking and
placing of the plunger into the channel.
[0197] FIG. 31 shows a reaction vessel 268 according to another
embodiment of the invention. The vessel 268 has a plunger 270 that
differs from the plunger of the preferred embodiment (described
above with reference to FIGS. 1-2). The plunger 270 includes a stem
272 and an elastomeric ring 274 encircling the stem 272. When the
plunger 270 is inserted into the channel 28, the ring 274
establishes a seal with the walls of the channel. With the seal
established, further insertion of the plunger 22 into the channel
28 compresses the air in the channel and creates the desired
pressurization of the chamber 17 (e.g., 2 to 50 psi above the
ambient pressure, or more preferably 8 to 15 psi above the ambient
pressure, as previously described in the preferred embodiment). The
walls of the channel 28 may have pressure control grooves if
desired, as explained above with reference to FIGS. 7A-7D, to
provide a controlled pressure stroke of the plunger 270.
Alternatively, the pressure control grooves may be omitted so that
the pressure stroke begins as soon as the ring 274 enters the
channel 28 and establishes a seal with the walls of the
channel.
[0198] The plunger 270 also includes two flanges 276A, 276B
extending radially from the stem 272. The flanges 276A, 276B are
positioned on opposite sides of the ring 274 to hold the ring in a
fixed position on the stem 272. The plunger 270 may optionally have
a head 278 at the end of the stem 272 for providing a physical
barrier against evaporation or reflux of the reaction mixture in
the chamber 17, similar to the tongue previously described with
reference to FIG. 29. With the exception of the elastomeric ring
274, the plunger 270 is preferably fabricated as a one-piece
polymeric part (e.g., polypropylene or polycarbonate) using known
injection molding processes. After the body of the plunger 270 is
molded, the ring 274 is stretched over the head 278 and positioned
on the stem 272 between the flanges 276A, 276B. The ring 274 may
comprise any suitable elastomeric material, e.g., a thermal plastic
elastomer (TPE) or silicone. As shown in FIG. 32, the plunger cap
280 may optionally include an engagement aperture 46 and alignment
apertures 48A, 48B to permit automated picking and placing of the
plunger into the channel.
[0199] FIG. 33 shows an alternative embodiment of the invention in
which the pressurization of the vessel 12 is performed by a
pick-and-place machine 282 having a machine head 284. The machine
head 284 has an axial bore 286 for communicating with the channel
28. The pick-and-place machine 282 also includes a regulated
pressure source in fluid communication with the bore 286 for
pressurizing the vessel 12 through the bore 286. The pressure
source may comprise, e.g., a syringe pump, compressed air source,
pneumatic pump, or connection to an external air supply.
[0200] The apparatus also preferably includes a disposable adapter
288 for placing the bore 286 in fluid communication with the
channel 28. The adapter 288 has an axial bore 290 that connects the
bore 286 in the machine head to the channel 28 in the vessel. The
adapter 288 is sized to be inserted into the channel 28 such that
the adapter establishes a seal with the walls of the channel. The
adapter 282 preferably comprises an elastomeric material, e.g., a
thermal plastic elastomer (tpe) or silicone. The adapter 288
preferably includes a one-way valve 292 (e.g., a check valve) for
preventing fluid from escaping from the vessel 12.
[0201] In operation, the vessel 12 is preferably placed into a
heat-exchanging module and filled with a reaction mixture as
previously described in the preferred embodiment. The vessel may be
filled manually by a human operator, or alternatively, the
pick-and-place machine 282 may include a pipette for filling the
vessel. After the chamber 17 is filled with the reaction mixture,
the machine head 284 picks up the adapter 288 and inserts the
adapter into the channel 28. To pick and place the adapter 288, the
machine head 284 preferably has a collet for gripping and releasing
the adapter 288. Alternatively, the machine head may be sized to
establish a press or friction fit with the adapter 288. When
inserted into the channel 28, the adapter 288 establishes a seal
with the walls of the channel. The pick-and-place machine 282 then
transmits gas, preferably air, from the pressure source into the
channel 28 to increase the pressure in the chamber 17. The flow of
air into the vessel 12 is stopped when the desired pressurization
of the chamber 17 is achieved.
[0202] The desired pressurization of the chamber 17 in this
embodiment is the same as that described in the preferred
embodiment above. As shown in FIG. 5, the pressure in the chamber
17 should be sufficiently high to ensure that the flexible major
walls 18 of the chamber outwardly expand to contact and conform to
the surfaces of the plates 50A, SOB. The pressure should not be so
great, however, that the walls 18 burst, become unattached from the
frame 16, or deform the frame or plates. It is presently preferred
to pressurize the chamber 17 to a pressure in the range of 2 to 50
psi above ambient pressure. This range is preferred because 2 psi
is generally enough pressure to ensure conformity between the
flexible walls 18 and the surfaces of the plates 50A, 50B, while
pressures above 50 psi may cause bursting of the walls 18 or
deformation of the frame 16 or plates 50A, 50B. More preferably,
the chamber 17 is pressurized to a pressure in the range of 8 to 15
psi above ambient pressure. This range is more preferred because it
is safely within the practical limits described above to allow for
any manufacturing or operational deviations from specification.
[0203] Referring again to FIG. 33, the machine head 284 is
disengaged from the adapter 288 following the pressurization of the
vessel 12. When the machine head 284 is disengaged from the adapter
288, the valve 292 prevents fluid from escaping from the vessel 12.
Thus, the chamber 17 remains pressurized for thermal processing and
the vessel 12 is effectively sealed to prevent the reaction mixture
in the vessel from contaminating the external environment. The
remaining operation of this embodiment is analogous to the
operation of the preferred embodiment described above.
[0204] FIG. 34 shows another embodiment of the invention in which
the filling and pressurization of vessel 12 is performed by a
pick-and-place machine 300 having a machine head 302 for
manipulating a needle 306. The machine head 302 has an axial bore
304 for communicating with the needle 306. The pick-and-place
machine 300 has controllable vacuum and pressure sources in
communication with the bore 304 for aspirating and dispensing
fluids using the needle 306. The vacuum and pressure sources may
comprise, e.g., one or more syringe pumps, compressed air sources,
pneumatic pumps, vacuum pumps, or connections to external sources
of pressure. The machine head 302 engages the needle 306 using any
standard needle fitting, such as a luer lock. The needle 306 is
preferably a double-bore needle having a first bore 308A for
injecting fluid into the vessel 12 and a second bore 308B for
venting gas from the vessel. For reasons that will soon be
apparent, the first bore 308A has a length greater than the second
bore 308B.
[0205] The apparatus also includes an elastomeric plug 310 that is
inserted into the channel 28 of the vessel such that the plug forms
a seal with the walls of the channel. The needle 306 is inserted
through the plug 310 by the machine head 302 to fill and pressurize
the chamber 17. The elastomeric plug 310 should be self-sealing so
that it seals fluid within the vessel 12 when the needle 306 is
withdrawn from the plug 310. The plug 310 is preferably inserted
into the channel 28 during manufacture of the vessel 12.
Alternatively, the plug 310 may be inserted into the channel 28
just prior to using the vessel 12, e.g., the plug may be inserted
by a robotic arm or machine tip of the pick-and-place machine 300
or the plug may be manually inserted by a human operator.
[0206] In operation, the vessel 12 is preferably placed into a
heat-exchanging module as previously described in the preferred
embodiment, e.g., by the pick-and-place machine 300 or by human
hands. The vessel 12 is then filled and pressurized by the
pick-and-place machine 300 as follows. The machine head 302 picks
up the needle 306 and aspirates the reaction mixture into the
needle through the first bore 308A. The machine head 302 then
inserts the needle through the plug 310 such that the first bore
308A is in fluid communication with the channel 28 and such that
the second bore 308B has one end disposed in the channel 28 and a
second end positioned outside of the vessel 12 and plug 310. The
pick-and-place machine 300 then dispenses the reaction mixture into
the chamber 17 through the first bore 308A of the needle. As the
chamber 17 is filled, displaced air in the vessel 12 is vented to
the atmosphere through the second bore 308B.
[0207] As shown in FIG. 35, the machine head 302 then partially
retracts the needle 306 from the plug 310 after the chamber 17 is
filled with the reaction mixture. The needle 306 is partially
retracted such that the end of the first bore 308A is still in
fluid communication with the channel 28, but the end of the second
bore 308B is enclosed within the plug 310. In this position, the
second bore 308B can no longer vent air from the channel 28. The
pick-and-place machine 300 then flows gas, preferably air, from the
controllable pressure source into the channel 28 through the first
bore 308A to increase pressure in the chamber 17. The machine 282
then stops the flow of air when the desired pressurization of the
chamber 17 is achieved.
[0208] The desired pressurization of the chamber 17 in this
embodiment is the same as that described in previous embodiments,
e.g., 5 to 50 psi and more preferably 8 to 15 psi for the reasons
discussed above. Following pressurization, the machine head 302
fully retracts the needle 306 from the plug 310, and the plug 310
self seals to maintain the desired pressure in the vessel 12 for
thermal processing. The needle 306 is preferably disposable to
prevent cross contamination of fluid samples. The remaining
operation of this embodiment is analogous to the operation of the
preferred embodiment described above.
[0209] FIG. 36 shows a slightly different embodiment of the
invention in which the machine head 302 manipulates a single-bore
needle 312 to fill and pressurize the chamber 17 in a single step.
In operation, the machine head 302 picks up the needle 312 and
aspirates the reaction mixture into the needle. The machine head
302 then inserts the needle 312 through the plug 310 and dispenses
the reaction mixture into the chamber 17. It is presently preferred
that the chamber 17 be filled from the bottom up by initially
inserting the needle 312 close to the bottom of the chamber 17 and
by slowly retracting the needle as the chamber 17 is filled.
Filling the chamber 17 in this manner reduces the likelihood that
air bubbles will form in the chamber.
[0210] Referring to FIG. 37, as the reaction mixture is added to
the chamber 17, the mixture displaces air in the vessel. The
displaced air is trapped between the liquid surface level S and the
plug 310 so that the air compresses in the channel 28. The
compression of the air is usually sufficient to cause the desired
pressurization of the chamber 17, e.g., 2 to 50 psi above the
ambient pressure, and more preferably 8 to 15 psi above the ambient
pressure. Thus, the filling of the chamber 17 also provides for
quick and convenient pressurization in a single step.
Alternatively, the pick-and-place machine 300 may be programmed to
increase or decrease the pressure in the vessel 12 by adding air to
the channel 28 or releasing air from the channel through the needle
312, as appropriate, to achieve the desired pressure in the chamber
17. The machine 300 preferably includes a pressure regulator for
this purpose. Suitable pressure regulators are well known in the
art.
[0211] After the desired pressurization of the chamber 17 is
achieved, the machine head 302 retracts the needle 312 from the
plug 310, and the plug 310 seals itself to maintain the pressure in
the vessel 12 for thermal processing. Many variations to this
embodiment are possible. For example, there may be low pressure or
a vacuum in the vessel 12 prior to adding the reaction mixture to
the chamber 17. To fill and pressurize the chamber 17, the
pick-and-place machine 300 first dispenses the reaction mixture
into the chamber 17 through the needle 312 and retracts the end of
the needle into the channel 28. The machine 300 then flows air from
the controllable pressure source into the channel 28 through the
needle 312 to achieve the desired pressurization of the chamber 17.
The machine head 302 then retracts the needle 312 from the plug
310, and the plug 310 seals itself to maintain the pressure in the
vessel 12 for thermal processing. The remaining operation of this
embodiment is the same as the operation of the preferred embodiment
described above.
[0212] FIG. 38 shows another embodiment of the invention in which
the sealing and pressurization of vessel 12 is performed by a press
314 having a heated platen 316 for heat sealing a film or foil 318
to the portion of the frame 16 forming the port 14. The foil 18 is
preferably a laminate comprising a layer of metal (e.g., aluminum)
on top of a layer of polymeric material (e.g., polypropylene or
polyester). In operation, the vessel 12 is preferably placed in a
holder (e.g., a tray or nest) that moves on an assembly line for
automated filling, sealing, and pressurization of the vessel. In a
first step, the chamber 17 of the vessel is filled with a reaction
mixture using, e.g., a pipette or syringe. After the chamber 17 is
filled, the foil 318 is placed on top of the port 14 with the metal
layer facing up. The foil 318 may be placed on the vessel manually
by a human operator, or more preferably, by the robotic arm of a
pick-and-place machine. The vessel 12 is then moved under the
heated platen 316 for sealing and pressurization. The platen 316 is
then pressed to the top of the vessel 12 and the platen 316 heat
seals the foil 318 to the vessel to seal the port 14.
[0213] As shown in FIG. 39, the heat from the platen 316 also melts
the top portion of the frame 16, thereby collapsing an end of the
channel 28 to produce a collapsed zone 319. The volume of the
channel 28 is therefore reduced. The reduction of the volume of the
channel 28 after the port is sealed compresses air trapped in the
channel and causes the desired pressurization of the chamber 17.
The desired pressurization of the chamber 17 in this embodiment is
the same as that described in the previous embodiments, e.g., 2 to
50 psi above the ambient pressure, and more preferably 8 to 15 psi
above the ambient pressure. After the vessel 12 is sealed and
pressurized in this manner, it is picked and placed into one of the
heat-exchanging modules 60 (FIG. 20) for thermal processing and
optical detection. The remaining operation of this embodiment is
the same as the operation of the preferred embodiment described
above.
[0214] The desired pressurization of the chamber 17 may be achieved
by use of the equation:
P.sub.i*V.sub.i=P.sub.f*V.sub.f;
where: P.sub.i is equal to the initial pressure in the vessel 12
prior to sealing the port; V.sub.i is equal to the initial volume
of the channel 28 prior to collapsing an end of the channel;
P.sub.f is equal to the desired final pressure in the chamber 17;
and V.sub.f is equal to the final volume of the channel 28 after
collapsing an end of the channel.
[0215] To ensure the desired final pressure P.sub.f in the chamber
17, the heat-sealing of the vessel should reduce the volume of the
channel 28 such that the ratio of the volumes V.sub.i:V.sub.f is
substantially equal to the ratio of the pressures P.sub.f:P.sub.i.
An engineer having ordinary skill in the art will be able to select
suitable values for the volumes V.sub.i and V.sub.f using the
description and equation given above. For example, if the initial
pressure Pi in the vessel is equal to standard atmospheric pressure
of about 14 psi, the desired final pressure P.sub.f is equal to 26
psi (the desired 12 psi above ambient pressure), and the initial
volume V.sub.i of the channel is equal to 150 .mu.l, then the heat
sealing of the vessel should reduce the volume of the channel to a
final volume V.sub.f of about 80 .mu.l. This is just one example of
suitable values for the initial and final volumes, and it is to be
understood that the scope of the invention is not limited to this
example. Many other suitable values may be selected to achieve the
desired ratios, as will be apparent to one having ordinary skill in
the art.
[0216] The various embodiments of the apparatus of the present
invention may find use in many applications. The apparatus may be
utilized to perform chemical reactions on samples, e.g., nucleic
acid amplification, and to optically detect amplified target
sequences. Although amplification by PCR has been described herein,
it will be appreciated by persons skilled in the art that the
apparatus may be utilized for a variety of other polynucleotide
amplification reactions and ligand-binding assays. Such additional
reactions may be thermally cycled or they may be carried out at a
single temperature, e.g., isothermal nucleic acid amplification.
Polynucleotide amplification reactions that may be practiced in the
system of the invention include, but are not limited to: (1) target
polynucleotide amplification methods such as self-sustained
sequence replication (3 SR) and strand-displacement amplification
(SDA): (2) methods based on amplification of a signal attached to
the target polynucleotide, such as "branched chain" DNA
amplification; (3) methods based on amplification of probe DNA,
such as ligase chain reaction (LCR) and QB replicase amplification
(QBR); (4) transcription-based methods, such as ligation activated
transcription (LAT) and nucleic acid sequence-based amplification
(NASBA); and (5) various other amplification methods, such as
repair chain reaction (RCR) and cycling probe reaction (CPR). Other
applications of the apparatus are intended to be within the scope
of the invention where those applications require the transfer of
thermal energy to a reaction mixture and/or optical detection of
reaction products.
SUMMARY, RAMIFICATIONS, AND SCOPE
[0217] Although the above description contains many specificities,
these should not be construed as limitations on the scope of the
invention, but merely as examples of some of the presently
preferred embodiments. Many modifications or substitutions may be
made to the apparatus and methods described without departing from
the scope of the invention. For example, in one alternative
embodiment, the reaction vessel has only one flexible sheet forming
a major wall of the reaction chamber. The rigid frame defines the
other major wall of the chamber, as well as the side walls of the
chamber. In this embodiment, the major wall formed by the frame
should have a minimum thickness of about 0.05 inches (the practical
minimum thickness for injection molding), while the flexible sheet
may be as thin as 0.0005 inches. The advantage to this embodiment
is that the manufacturing of the reaction vessel is simplified, and
hence less expensive, since only one flexible sheet need be
attached to the frame. The disadvantage is that the heating and
cooling rates of the reaction mixture are likely to be slower since
the major wall formed by the frame will probably not permit as high
a rate of heat transfer as the thin, flexible sheet.
[0218] In addition, the apparatus only requires one thermal surface
for contacting a flexible wall of the reaction vessel and one
thermal element for heating and/or cooling the thermal surface. The
advantage to using one thermal surface and one thermal element is
that the apparatus may be manufactured less expensively. The
disadvantage is that the heating and cooling rates are likely to be
about twice as slow. Further, although it is presently preferred
that the thermal surfaces be formed by thermally conductive plates,
each thermal surface may be provided by any rigid structure having
a contact area for contacting a wall of the vessel. The thermal
surface preferably comprises a material having a high thermal
conductivity, such as ceramic or metal. Moreover, the thermal
surface may comprise the surface of the thermal element itself. For
example, the thermal surface may be the surface of an ultrasonic
transducer that contacts the flexible wall of the chamber for
ultrasonic heating and/or lysing of the sample in the chamber.
Alternatively, the thermal surface may be the surface of a
thermoelectric device that contacts the wall to heat and/or cool
the chamber.
[0219] The filters used in the optics assemblies may be designed to
provide excitation and emission light in any wavelength ranges of
interest, not just the specific wavelength ranges described above.
The choice of fluorescent dyes for any given application depends
upon the analytes of interest. One skilled in the art will realize
that different combinations of light sources, filters, or filter
wavelengths may be used to accommodate the different peak
excitation and emission spectra of the selected dyes. Moreover,
although blue and green light sources are presently preferred,
different color light sources, such as blue-green, red, or amber
LEDs, may be used in the apparatus. Further, infrared or
ultraviolet light sources may be used.
[0220] Moreover, although fluorescence excitation and emission
detection is a preferred embodiment, optical detection methods such
as those used in direct absorption and/or transmission with on-axis
geometries may also be applied to the apparatus of the present
invention. Alternative geometries, such as on-axis alignments of
light sources and detectors, can be used to monitor changes in dye
concentrations and physical conditions (temperature, pH, etc.) of a
reaction by measuring absorption of the illumination. The optics
may also be used to measure time decay fluorescence. Additionally,
the optics are not limited to detection based upon fluorescent
labels. The optics system may be applicable to detection based upon
phosphorescent labels, chemiluminescent labels, or
electrochemiluminescent labels.
[0221] Therefore, the scope of the invention should be determined
by the following claims and their legal equivalents.
* * * * *