U.S. patent number 3,901,798 [Application Number 05/417,886] was granted by the patent office on 1975-08-26 for aerosol concentrator and classifier.
This patent grant is currently assigned to Environmental Research Corporation. Invention is credited to Carl M. Peterson.
United States Patent |
3,901,798 |
Peterson |
August 26, 1975 |
Aerosol concentrator and classifier
Abstract
An aerosol sampler which concentrates and classifies airborne
particles. Particles in the size range of 0.1 - 10 microns are
classified according to particle size by means of the particle
inertia principle. The unique design reduces particle losses and is
characterized by an annular passage in the flow path of the
sample.
Inventors: |
Peterson; Carl M. (St. Paul,
MN) |
Assignee: |
Environmental Research
Corporation (St. Paul, MN)
|
Family
ID: |
23655766 |
Appl.
No.: |
05/417,886 |
Filed: |
November 21, 1973 |
Current U.S.
Class: |
209/143; 73/865;
73/865.5 |
Current CPC
Class: |
B07B
7/02 (20130101) |
Current International
Class: |
B07B
7/00 (20060101); B07B 7/02 (20060101); B07B
007/00 () |
Field of
Search: |
;209/143,145,1,210
;73/28,29,432PS,421.5R ;55/270,319,434,439,17 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
|
|
|
|
|
|
|
1,593,451 |
|
Jul 1970 |
|
FR |
|
1,015,882 |
|
Jan 1966 |
|
GB |
|
Primary Examiner: Lutter; Frank W.
Assistant Examiner: Hill; Ralph J.
Attorney, Agent or Firm: Dorsey, Marquart, Windhorst, West
& Halladay
Claims
I claim as my invention:
1. Apparatus for classifying airborne particles according to
particle size which comprises:
a first plate defining a first orifice;
a second plate spaced from the first plate and defining a second
orifice larger than and substantially concentrically disposed with
respect to the first orifice;
tubular means defining a third orifice disposed substantially in
the plane of the second orifice, directed toward, substantially the
size of, and substantially concentrically disposed with respect to
the first orifice, to thereby define an annular passage between the
second orifice and the tubular means;
means for establishing communication between said first orifice, on
the one hand, and said third orifice and said annular passage, on
the other hand;
an outlet for returning air passing through said annular passage to
the atmosphere;
means for establishing communication between said annular passage
and said outlet; and
collecting means communicating with the third orifice for
collecting the particles passing therethrough.
2. The apparatus of claim 1 and means for providing a pressure
gradient decreasing in pressure from the first orifice to the
annular passage and the third orifice.
3. The apparatus of claim 1 wherein the first orifice is
substantially circular.
4. The apparatus of claim 3 wherein the spacing between the first
plate and the second plate of 0.3 - 3 times the diameter of the
first orifice.
5. The apparatus of claim 4 wherein the distance between the
annular passage and the third orifice is equal to or less than
one-half the diameter of the first orifice.
6. The apparatus of claim 5 wherein the area of the annular passage
is 0.6 - 1 times the area of the first orifice.
7. The apparatus of claim 6 wherein the thickness of the first
plate is less than or equal to the diameter of the first
orifice.
8. The apparatus of claim 1 and secondary stage classifying means
comprising:
a secondary first plate defining a secondary first orifice disposed
in the path of the particles after passage through the third
orifice and prior to entrance into the collecting means;
means for establishing communication between said third orifice and
said secondary first orifice;
a secondary second plate spaced from the secondary first plate and
defining a secondary second orifice larger than and substantially
concentrically disposed with respect to the secondary first
orifice; and
secondary tubular means defining a secondary third orifice
communicating with the collecting means and disposed substantially
in the plane of the secondary second orifice, directed toward,
substantially the size of, and substantially concentrically
disposed with respect to the secondary first orifice to thereby
define a secondary annular passage between the secondary second
orifice and the secondary tubular means;
means for establishing communication between said secondary first
orifice, on the one hand, and said secondary third orifice and said
secondary annular passage, on the other hand; and
means for establishing communication between said secondary annular
passage and said outlet.
9. The apparatus of claim 8 and means for providing a pressure
gradient decreasing in pressure from the first orifice to the
annular passage and the third orifice, from the third orifice to
the secondary first orifice, and from the secondary first orifice
to the secondary annular passage and the secondary third
orifice.
10. The apparatus of claim 9 wherein the secondary first orifice is
substantially circular.
11. The apparatus of claim 10 wherein the spacing between the
secondary first plate and the secondary second plate is 0.3 - 3
times the diameter of the secondary first orifice.
12. The apparatus of claim 11 wherein the distance between the
secondary annular passage and the secondary third orifice is equal
to or less than one-half the diameter of the first orifice.
13. The apparatus of claim 12 wherein the area of the annular
passage is 0.6 - 1 times the area of the secondary first
orifice.
14. The apparatus of claim 13 wherein the thickness of the
secondary first plate is less than or equal to the diameter of the
secondary first orifice.
Description
BACKGROUND OF THE INVENTION
The invention pertains to the field of analyzing particle laden (or
polluted) air by measuring the concentration, size and size
distribution of the suspended particles. It is useful in the
detection of biological or radioactive particles suspended in the
atmosphere, in the detection of biological contamination in
hospitals, in the analysis of smoke stack emissions, in monitoring
ambient conditions for pollution, and in classification of pigments
according to particle size. In general the invention is useful in
any field which requires the sampling, concentrating, or
classifying according to particle size, of nonfibrous airborne
particles within the size range of 0.1 - 10 microns.
The invention operates on the principle of particle inertia. Air
with suspended particles is caused to flow along a path, and a
portion of the airstream is deflected. The smaller particles with
less mass and inertia negotiate the turn and continue along the
deflected path. The larger particles (above the cutpoint) with
greater mass and inertia fail to negotiate the turn and continue
along the original direction of the airstream. Particles are thus
separated or classified according to particle size.
The effect and persistence of particulate matter in the atmosphere
is primarily dependent upon particle size. Reduction in atmospheric
visibility, for example, is largely due to particles in the size
range of 0.1 - 1 microns. Where synergistic action has been
observed with toxic gases, indications are that the effect is more
pronounced when the particles are submicron in size. Particulates
of definable particle size enhance atmospheric reactions and
transformations of pollutant gases, exert an influence on radiation
transfer of solar energy to the earth's surface, and may be
responsible for inadvertent weather modification by nucleating
cloud formation. Accordingly, air quality and source emission
standards will likely be expressed in terms of the size of emitted
particles and, consequently, means for measuring and classifying
particles according to particle size will be required.
The principle of particle inertia has been used in prior art
devices. The cascade impactors described by Hounam and
Sherwood.sup.1, and by Connor.sup.2, for example, utilize this
principle. In these, as well as other prior art devices, particle
wall losses are significant, that is, 40-45% particle loss or
55-60% efficiency is not uncommon when comparing what comes out
with what goes in. In addition in prior art devices there is
substantial particle bounce-off from the collected surfaces which
distorts the particle size distribution of the sample collected.
Moreover, the limited quantity of particle mass which can be
collected prior to particle reentrainment is another limitation of
prior art devices, and the collection surface upon which the
particles are collected in prior art devices is not readily
amenable to a variety of analysis techniques including
beta-attenuation, culturing, microscopic examination, and other
methods.
SUMMARY OF THE INVENTION
The primary advantage of the present invention is that particle
losses are reduced to 15-20%, that is, the sampler operates at an
efficiency in the range of 80-85%. In addition the present
invention promotes efficient impingement and concentration of
particles of various sizes into a given classification, that is, a
more precise cutpoint for particles of various sizes results. The
present invention also facilitates removal of the sample onto a
defined filter media or area for analysis.
The invention is characterized by an annular passage disposed about
and in the plane of a second orifice concentrically located in
spaced relationship downstream from a first orifice.
More particularly, the invention may be summarized as apparatus for
classifying airborne particles according to particle size including
a first plate which defines a first orifice. A second plate spaced
from the first plate defines a second orifice larger than and
substantially concentrically disposed with respect to the first
orifice. The second orifice is downstream from the first. Tubular
means, also downstream from the first orifice, disposed
substantially in the plane of the second orifice, directed toward,
substantially the size of, and substantially concentrically
disposed with respect to the first orifice, defines a third orifice
and an annular passage between the second orifice and tubular
means. This annular passage is the critical element in the present
invention and distinguishes it from prior art devices. A pressure
gradient, decreasing in pressure from the first orifice to the
annular passage and third orifice is provided to induce flow
through the first orifice and the third orifice and the annular
passage. In the embodiment shown the first orifice, the third
orifice, and the annular passage are circular.
The invention may be practiced in a plurality of stages. For this
purpose, second stage classification apparatus may be disposed in
the airstream that passes through the third orifice in the first
stage. Additional stages may also be provided.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view of the preferred embodiment showing
the intake section, the first stage section, the second stage
section, and the blower section.
FIG. 2 is a top view of the aerosol sampler shown in FIG. 1.
FIG. 3 is a vertical sectional view of the present invention taken
on the line 3--3 of FIG. 2.
FIG. 4 is a horizontal sectional view taken on the line 4--4 of
FIG. 3.
FIG. 5 is a horizontal sectional view taken on the line 5--5 of
FIG. 3.
FIG. 6 is an enlarged, schematic, vertical sectional view of the
classification zone of the present invention. The relative size and
relationship of the critical elements is shown.
FIG. 7 is an enlarged, schematic, vertical sectional view similar
to FIG. 6 and shows a second stage classification section.
DESCRIPTION OF THE PREFERRED EMBODIMENT
The general nature of the present invention may be readily
understood with reference to FIG. 1. Ambient air to be concentrated
and classified enters the aerosol sampler 10 at intake section 11.
The sample passes downwardly through first stage section 13 in
which fractionation occurs and then through second stage section 14
in which further fractionation occurs. The sample fraction is
collected in second stage section 14. The balance and major
volumetric portion of the airstream passes through blower section
15, and exits from the apparatus at exhaust cylinder 16. Timer 17
serves to record the length of time of operation of the apparatus
or the length of time over which the sample is collected. The
classification of particles in the airstream is brought about
between intake section 11 and exhaust cylinder 16 in a manner
described in detail below.
The detailed design and construction of the present invention may
be readily understood with reference primarily to FIGS. 2-6. With
reference first to FIG. 3, intake section 11 includes flow
containment collar 20 which is generally cylindrical and flanged at
one end. With continued reference to FIG. 3, first stage section 13
includes cylindrical housing 21 which is internally flanged at its
upper edge and externally flanged at its lower edge. Nozzle orifice
plate 22, guide plate 23, separation plate 24, and first stage
collecting cavity housing 25 complete the basic elements in first
stage section 13. Nozzle orifice plate 22 defines a series of
spaced orifices 26 shown in both FIGS. 3 and 4. Orifices 26, which
constitute the first orifice in the path of the airstream, are
radially disposed about the vertical axis of sampler 10 and, in the
preferred embodiment shown, number 30. A similar number of orifices
27 are provided in guide plate 23. These orifices 27 are larger
than and concentrically disposed with respect to nozzle orifices
26, and are spaced downstream therefrom. Orifices 27 constitute the
second orifice in the path of the airstream. A similar number of
tubular or third orifices 28 are defined by separation plate 24 as
best seen in FIG. 3. The third orifices 28 are spaced from first
orifices 26, downstream therefrom, and are disposed concentrically
with respect thereto in the plane of second orifices 27. The wall
of tubular orifices 28 is sufficiently thin so that the outside
diameter of the tubular portion is less than the diameter of the
second orifices 27. Thus, an annular passage 30 is formed between
second orifice 27 and the outer wall of third or tubular orifice
28. This annular passage 30 may be seen with reference to FIGS. 3,
5 and 6 and characterize the invention.
First stage collection cavity housing 25 has an open top surface
and defines air cavity 31 which serves as a confinement area for
that portion of the airstream and fractionated airborne particles
which pass through each third orifice 28. First stage collecting
cavity 25, together with first stage cylindrical housing 21,
defines an annular cavity 32 which serves as a confinement area for
that portion or fraction of the airstream and airborne particles
which pass through each annular passage 30.
Intake section 11 is mounted to first stage section 13 by means of
screws 35. Nozzle orifice plate 22, gasket 29, guide plate 23, and
separation plate 24, are held in the requisite relationship and
connected to first stage collection cavity housing 25 by means of
screws 36.
Second stage section 14 begins with mounting plate 40 and
separation plate 41 which defines large unrestricted passages 42.
Sample collector 43, sample collector mounting sleeve 44, and
second stage cylindrical housing 45 are also provided in second
stage section 14. Cylindrical housing 45, formed from rigid
transparent material, is mounted to separation plate 41 and
mounting plate 40 by means of screws 46 which extend through lower
separation plate 47 and are threaded into mounting plate 40. Second
stage section 14 is mounted to first stage section 13 by means of
mounting plate 40 which is mounted and sealed to the lower flange
of first stage cylindrical housing 21 by means of screws 50 and
O-ring 51.
Liquid or culture medium input tube 53 extends through second stage
cylindrical housing 45 and connects with sample collector 43 at
mounting tube 54. Sample collection tube 55 extends from downwardly
projecting mounting tube 56 of sample collector 43 and outwardly
through second stage cylindrical housing 45, as best seen in FIG.
3.
The second stage concentration and classification occurs at
secondary orifices 60 disposed in the bottom plate portion of first
stage collection cavity housing 25. Concentrically disposed second
stage orifices 61 in the upper portion of the sample collector 43,
along with annular passage 32, serve to classify the airstream
further, that is, accomplish a secondary classification, as the
once fractionated airstream from air cavity 31 passes through
orifices 60 and is further concentrated and classified. A portion
of the stream passes into annular cavity 32 and through large
unrestricted passages 42, while the other portion passes through
orifices 61 into sample collector 43. It may be noted at this point
that the secondary concentration and classification shown in FIG. 3
does not include the characteristic annular passage described above
in connection with the first stage classification. While not shown,
a similar secondary classification structure could be provided in
the second stage and, moreover, such an arrangement is shown
schematically in FIG. 7.
With continued reference to FIG. 3, blower section 15 includes
cylindrical blower housing 70, under separation plate 71 which
defines a centrally disposed unrestricted passage 72, squirrel cage
73 keyed to drive shaft 74, intermediate separation plate 75 which
defines unrestricted passage 76, motor 77, and bottom plate 78.
Bottom plate 78 is mounted to cylindrical blower housing 70 by
means of the screws 79. Exhaust cylinder 16, formed integrally with
cylindrical blower housing 70, completes blower section 15. A
conventional timer 17 (shown in FIG. 1) is mounted to blower
housing 70 to record the length of time over which the sample is
collected.
The relative size of the critical parts of the invention may be
best understood with reference to FIG. 6. The same reference
numerals used in describing the preferred embodiment of FIGS. 1-5
are applied to the corresponding elements shown schematically in
FIG. 6. With reference to FIG. 6, the distance, D, between first
plate 22 and second plate 23 should be 0.3 - 3 times the diameter,
d.sub.1, of first orifice 26. The width, w, of annular passage 30
should be equal to or less than one-half the diameter, d.sub.1, of
first orifice 26. The diameter, d.sub.2, of third orifice 28 should
be equal to or slightly less than the diameter, d.sub.1, of first
orifice 26. The diameter of second orifice 27, and the wall
thickness of tubular orifice 28, should be such that the area of
the annular passage 30 is 0.6 - 1 times the area of third orifice
28. The thickness, t, of first plate 22 should be less than the
diameter, d.sub.1, of first orifice 26. For a concentration ratio
(by volume) of 8:1, the area of annular passage 30 should be 0.8
times the area of third orifice 28. For fractionation of particles
in the size range of 0.1 - 10 microns, the diameter, d.sub.1, of
first orifice 26 should be in the range of 0.2 - 0.5 inches.
For a 50% cutpoint of 1.5 microns.sup.1, the diameter, d.sub.1, of
first orifice 26 should be 0.136 inches. The pressure, P.sub.ann,
in annular passage 30 and annular cavity 32 should be 16-18 inches
of water less than atmospheric pressure, P.sub.atn. The pressure,
P.sub.cav, in third orifice 28 and first stage collection cavity 31
should be only slightly less than atmospheric, that is, 0.1 - 0.2
inches of water less than atmospheric, P.sub.atm. Under the
foregoing conditions, the velocity of the airstream passing through
first orifice 26 is approximately 6,200 centimeters per second. The
volumetric through-put is about 35 cfm. Those skilled in the art
may choose a blower and motor of appropriate size and capacity to
achieve these conditions.
The operation of the invention may be best understood with
reference to FIG. 7. A two stage classifier is shown schematically
in FIG. 7 and the elements or components are assigned reference
numerals identical to the numerals assigned to the corresponding
elements or components shown or described in connection with the
preferred embodiment in FIGS. 1-5. Due to the pressure gradient
referred to above in the description of the preferred embodiment,
ambient air, that is, the air to be sampled, is drawn into intake
section 11 and into orifices 27. At this point fractionation
occurs. A portion of the airstream, that is, approximately 80-90%
by volume of the airstream, is deflected and passes through annular
passage 30 into annular cavity 32. The balance of the airstream,
that is, 10-20% by volume, passes directly from first orifice 27
through third orifice 28 and into first stage collecting cavity 31.
The difference in volume when comparing the volume of the airstream
passing through annular passage 30 with the volume passing through
third orifice 28 is due to the substantial difference between the
pressure in annular cavity 32 and first stage collection cavity 31.
In other words, the pressure gradient from first orifice 27 to
annular passage 30 and annular cavity 32 is substantial, whereas
the pressure gradient between first orifice 27 and third orifice 28
is slight. Fractionation occurs as the airstream is deflected from
a path directly from first orifice 27 through third orifice 28 with
a substantial portion passing through annular passage 30. At this
point particles above the cutpoint continue along a path without
deflection and in first stage collection cavity 31. Particles below
the cutpoint negotiate the turn, due to their smaller mass and
inertia, and pass through annular passage 30 and enter annular
cavity 32. Further fractionation occurs at second stage orifice 60.
The nature of the classification in the second stage is identical
to that in the first. The fraction of air in annular cavity 32
resulting from both first and second stage classification is
discharged through exhaust cylinder 16. The sample fraction is
collected on sample collector 43 and analyzed. Analysis may be
carried out by beta-attenuation, by culturing the sample, and by
other means known to those skilled in the art.
* * * * *