U.S. patent number 3,807,403 [Application Number 05/262,543] was granted by the patent office on 1974-04-30 for cryosurgical apparatus.
This patent grant is currently assigned to Frigitronics of Conn. Inc.. Invention is credited to Joseph F. Andera, Joseph C. Stumpf.
United States Patent |
3,807,403 |
Stumpf , et al. |
April 30, 1974 |
**Please see images for:
( Certificate of Correction ) ** |
CRYOSURGICAL APPARATUS
Abstract
There is disclosed a cryosurgical apparatus of the type which
operates from a source of compressed gas. It includes an improved
nozzle which is substantially less critical tnan prior art nozzles
and permits simplified and less expensive construction. A defrost
valve in the exhaust conduit permits easy and quiet operation by
the surgeon. An insulator tube is resiliently secured to the probe
to allow thermal expansion and contraction without stress. The
foregoing abstract is not to be taken either as a complete
exposition or as a limitation of the present invention. In order to
understand the full nature and extent of the technical disclosure
of this application, reference must be had to the following
detailed description and the accompanying drawings as well as to
the claims.
Inventors: |
Stumpf; Joseph C. (Fairfield,
CT), Andera; Joseph F. (Trumbull, CT) |
Assignee: |
Frigitronics of Conn. Inc.
(Skelton, CT)
|
Family
ID: |
22997946 |
Appl.
No.: |
05/262,543 |
Filed: |
June 14, 1972 |
Current U.S.
Class: |
606/26; 62/293;
62/51.1 |
Current CPC
Class: |
A61F
7/12 (20130101); A61B 18/02 (20130101); F25B
2309/021 (20130101); F25B 2309/022 (20130101) |
Current International
Class: |
A61B
18/00 (20060101); A61B 18/02 (20060101); A61F
7/12 (20060101); A61b 017/36 (); A61f 007/12 () |
Field of
Search: |
;62/293,514
;128/303.1,400,401 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Pace; Channing L.
Attorney, Agent or Firm: Buckles and Bramblett
Claims
We claim:
1. A gas operated cryosurgical instrument which comprises: a
tubular exhaust conduit terminating at one end in a hollow probe
tip of high thermal conductivity; a remote source of high pressure
gas; a gas delivery conduit extending through said exhaust conduit
in fluid flow communication with said source and terminating at a
nozzle within said probe tip; normally open valve means connected
in fluid flow relationship between said exhaust conduit and
atmosphere; and means for controllably closing and opening said
valve means.
2. The instrument of claim 1 wherein said valve means comprises: a
stationary valve seat defined by said exhaust conduit; and a
moveable valve member carried by said delivery conduit.
3. The instrument of claim 2 wherein said closing means comprises a
manually operable trigger connected to advance both of said
delivery conduit and valve member.
4. A gas operated cryosurgical instrument which comprises: a
tubular exhaust conduit terminating at one end in a hollow probe
tip of high thermal conductivity; a gas delivery conduit extending
through said exhaust conduit and terminating at a nozzle within
said probe tip, said nozzle including a cylindrical gas discharge
passage of smaller diameter than said delivery conduit and a
smoothly curved reduction passage therebetween; normally open valve
means connected in fluid flow relationship between said exhaust
conduit and atmosphere; an insulator tube surrounding, but spaced
from, said exhaust conduit; resilient means interconnecting said
insulator tube and exhaust conduit; and means for controllably
closing and opening said valve means.
5. The instrument of claim 4 wherein said resilient means comprises
an annular bushing encircling said exhaust conduit adjacent said
probe tip and frictionally engaging both of said exhaust conduit
and insulator tube to permit relative motion therebetween.
6. The instrument of claim 5 wherein said probe tip includes a
substantially cylindrical stem and said insulator tube encircles
one end of said stem in sliding relationship therewith.
Description
BACKGROUND OF THE INVENTION
This invention pertains to cryosurgical instruments of the type
which are cooled under the influence of high pressure gas escaping
from an orifice. Instruments of this type are well known in the art
and are widely employed for a number of surgical procedures such as
the necrosis of diseased tissue. Several gases exhibit the Joule
Thomson effect and may be used in the operation of the instrument.
The most common, however, are nitrous oxide and carbon dioxide.
In instruments of this type, the gas expansion orifice is of an
extremely small size and in all prior art instruments the spacing
between the orifice and the inner wall of the cooling tip is
extremely critical. For example, with prior art instruments, the
orifice is positioned approximately 0.050 inch from the inner wall
of the tip and the permitted tolerance is only 0.010 inch. This
results in such instruments being difficult and costly to
manufacture. For example, the parts of such instruments are
commonly threaded so that they may be factory adjusted prior to
shipment.
Another problem connected with prior art instruments of this type
is found in the exhaust valve of intruments which have controlled
defrost. For example, one such instrument is normally warm, which
means that the exhaust valve is normally closed and the device is
filled with compressed gas at bottle pressure. As the bottle gas
prssure may be commonly as high as 800 psi, it will be quite
apparent that this creates an explosion hazard. The exhaust valve
used in this prior art device comprises a cylindrical piston which
seats against a small exhaust orifice and is retained in the seated
position by means of a heavy spring. The piston is raised against
the force of a spring by means of a finger operated toggle. When
the surgeon wishes to cool the probe tip, he must apply substantial
force to depress the toggle which is, itself, detrimental,
particularly in the case of very delicate surgical procedures.
Secondly, as soon as the piston begins to leave the orifice, the
full bottle pressure, which was formerly applied only to a small
area of the piston, is now applied to the full area of the piston
end, slamming the piston open with an explosive-like report.
Still another problem with prior art devices arises from the fact
that they are subject to considerable thermal stress. For example,
it is usually desirable to provide an insulated housing to prevent
adherence to healthy tissue. This housing should preferably remain
at room temperature. However, the tip and exhaust conduit may be
cooled to temperatures as low as -89.degree.C. The resultant
contraction may result in substantial stresses at the junctures of
the cold and warm parts.
Accordingly, it is a primary object of the present invention to
provide an improved cryosurgical instrument of the gas operated
type having much less critical tolerances, permitting it to be
assembled in a much less expensive manner such as by electron beam
welding. Other objects are to provide such an instrument which is
only intermittently exposed to full bottle gas pressure, which has
a substantially silent and easily operated exhaust valve, and which
has substantially no thermal stresses between the cooled parts and
the insulator housing. The manner in which these objects are
achieved will be apparent from the following description and
appended claims.
SUMMARY OF THE INVENTION
The invention comprises a gas operated cryosurgical instrument
including a tubular exhaust conduit terminating at one end in a
hollow probe tip of high thermal conductivity. A high pressure gas
delivery conduit extends through the exhaust conduit and terminates
at a nozzle within the probe tip. The nozzle has a cylindrical gas
discharge passage of smaller diameter than the delivery conduit and
a smoothly curved reduction passage therebetween. A normally open
valve is connected in fluid flow relationship with the exhaust
conduit. An insulator tube surrounds but is spaced from the exhaust
conduit and is connected thereto by a resilient connection.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a perspective view of a cryosurgical instrument in
accordance with the present invention shown connected to a source
of bottled gas;
FIG. 2 is an enlarged cross section taken through the instrument of
FIG. 1;
FIG. 3 is an enlarged cross section of the exhaust valve of FIG.
2;
FIG. 4 is a greatly enlarged cross section of the nozzle portion of
the apparatus;
FIG. 5 is an illustration of the gas jet obtained with the nozzle
of FIG. 4;
FIG. 6 is a cross section taken substantially along the line 6--6
of FIG. 5;
FIG. 7 is an illustration of one type nozzle used in the prior
art;
FIG. 8 is a cross section taken substantially along the line 8--8
of FIG. 7;
FIG. 9 is an illustration of another type of nozzle used in the
prior art;
FIG. 10 is an enlarged cross section showing the orifice of the
FIG. 9 nozzle;
FIG. 11 shows still another type of nozzle used in the prior
art;
FIG. 12 illustrates the resilient connection between the warm
insulator tube and the cold portions of the probe; and
FIG. 13 is an illustration similar to FIG. 12 showing the manner in
which the resilient connection operates.
DESCRIPTION OF THE PREFERRED EMBODIMENT
With particular reference to FIG. 1, there is disclosed an
instrument of the type utilized in treating cervicitis. It
comprises an elongated probe 10 mounted in a handle 12 and
terminating in a substantially conical applicator tip 14. The other
end of the probe extends from the handle and is connected to a line
16 which, in turn, is connected to a suitable source 18 of
pressurized gas. A trigger 20 extends from the handle for selective
defrosting as will be explained.
Turning now to FIG. 2, the handle 12 will be seen to support the
rear portion 22a of a stainless steel insulator tube 22. The rear
portion 22a and a forward portion 22b are each welded to the
circumferential flange 24 of an internally threaded sleeve 26.
Threaded into sleeve 26 is a bushing 28 which is welded to the end
of an exhaust tube 30. The end of exhaust tube 30 has a bevelled
valve seat 32 as shown in FIG. 3. The other end of exhaust tube 30
is welded to a bushing 34 which, in turn, is welded to the
cylindrical stem 36 of the hollow copper tip 14. The forward end of
the insulator tube 22 extends over the surface of stem 36 but is
not secured thereto. Instead, a resilient bushing 38 frictionally
engages both the exhaust tube 30 and the insulator tube 32.
The line 16 is a coaxial conduit comprising a silicon coated
fiberglass exhaust line 40 secured by a spring 42 to the end of
insulator tube 22. Carried within the exhaust line is a high
pressure delivery line 44 secured by means of a high pressure
connector 46 to the threaded end 48 of a steel valve member 50
which is illustrated in more detail in FIG. 3.
The valve member 50, in addition to the threaded end 48, has an
unthreaded forward portion 52 and a central circumferential flange
54. The forward surface of flange 54 carries a circular knife edge
56. A Teflon valve member 58 is press fitted over the forward
portion 52 and has a flat rear surface which engages the knife edge
56. The forward surface of valve seat 58 is tapered to engage the
valve seat 32 on exhaust tube 30. The upper end of trigger 20
defines a drilled opening 60 through which the threaded end 48 of
valve member 50 extends. It is held in place by a nut 62. The
trigger 20 is mounted on a pivot 64 positioned approximately one
inch below its upper end. The length of trigger 20 below the pivot
64 is approximately 4 inches in the described embodiment. Welded to
the unthreaded forward portion 52 of valve member 50 is the end of
a delivery tube 66 which in one embodiment is a 15 gauge stainless
steel hypodermic tube having an internal diameter of 0.059 inch.
The forward end of delivery tube 66 has a reduced diameter portion
forming a nozzle 68 positioned within the hollow probe tip 14.
The construction of nozzle 68 will be best understood by reference
to FIG. 4. As will be seen therein, the internal diameter of the
delivery tube 66 is reduced via a smooth wall reduction passage 70
to a cylindrical gas discharge passage 72. This configuration is
achieved by inserting into the end of the hypodermic tube a
hardened wire having an external diameter equal to the desired
diameter of the gas discharge passage. The end of the tube is then
swaged onto the wire and the wire is removed. In one actual
embodiment, the tube 66 has an internal diameter of 0.059 inch and
the internal diameter of the gas discharge passage 72 is 0.01065
inch. The distance from the nozzle to the beginning of reduction
("A" FIG. 4) is 0.20 inch and the distance between the nozzle tip
and the end of reduction ("B") is 0.12 inch.
The performance of the nozzle 68 is strikingly superior to those of
the prior art. The reason for this is not fully understood but is
believed to be due to the smooth continuous inner surface formed by
the reduction passage 70 and the gas discharge passage 72. This is
believed to prevent gas turbulence and permit laminar flow out of
nozzle 68.
FIG. 5 illustrates the gas flow from the nozzle 68 as actually
observed in practice. As will be seen, it presents an elongated
"flame like" appearance and shape. FIGS. 7-11 illustrate three
prior art nozzle constructions and the jets obtained thereby. FIGS.
7 and 8 illustrate a pinched tube configuration. FIGS. 9 and 10
illustrate a rolled end construction and FIG. 11 illustrates a type
of orifice known as a "double reduction" orifice which comprises a
series of tubes of reduced diameter. The jets from these prior art
nozzles appear as indicated. In these prior art nozzles the
distance from the orifice to the wall of the applicator tip is very
critical and the spacing must be quite close. As an example, this
distance may be 0.050 inch with a tolerance of + or - 0.010 inch.
In contrast, when utilizing the nozzle of this invention, the
distance from the nozzle tip to the wall may be 0.250 inch with a
tolerance of + or - 0.060 inch. Accordingly, by means of this
invention, manufacture and assembly are greatly simplified,
resulting in a highly effective instrument at a much lower
cost.
The resilient tip construction is illustrated in detail in FIGS. 12
and 13. As seen in FIG. 12, the insulator tube 22 is spaced from
exhaust tube 30, providing an insulating air space therebetween.
The end of the insulator tube 22 slidingly encircles the stem 36 of
tip 14. A resilient bushing 38 engages both the insulator tube and
the exhaust tube. As the probe tip is cooled, the tip 14 and the
exhaust line 30 will both cool and contract. This is shown in an
exaggerated manner in FIG. 13 wherein it will be seen that the
normal resilience of bushing 38 compensates for expansion and
contraction and prevents stresses from building up in the
instrument.
The nozzle and the resilient tip construction may be utilized in
connection with either a non-defrostable or a defrostable
cryosurgical probe. The probe illustrated herein is of the
defrostable type. Defrosting is obtained by means of the valve
illustrated in detail in FIG. 3. When the valve is in its normally
open position, high pressure gas entering through delivery line 44
passes through the hollow passage in the valve member 50 an through
delivery tube 66 to nozzle 68. From the nozzle it expands into tip
14, causing the tip to be cooled by the Joule Thomson effect. The
expanded gas then passes rearwardly through exhaust tube 30 and out
the exhaust line 40. It may then be exhausted to atmosphere through
any suitable opening such as the vent 74 shown in FIG. 1. The high
pressure exhaust gas tends to maintain the exhaust valve in its
normally open position without the need for springs or similar
devices. In order to defrost the instrument, the trigger 20 is
depressed by the surgeon, whereupon it assumes the dashed line
position illustrated in FIG. 2 and forces the Teflon valve member
58 against the bevelled valve seat 32 of the exhaust tube 30. The
circular knife edge 56 forms a gas tight seal with the rear of the
valve member. With the exhaust valve closed, the gas pressure
within tip 14 rises to bottle pressure and the heat of compression
causes rapid defrosting of the probe tip. In one embodiment, the
diameter of the valve member 58 which is exposed to gas pressure is
approximately 0.187 inch. With a bottle pressure of 800 psi, this
results in 27 pounds force tending to drive the valve member to the
rear. The 4:1 lever ratio of the trigger 20 results in only 6.8
pounds of force being required to close the valve and maintain it
in the closed position. As the valve is normally open, it will be
closed only for the period of time during which the surgeon desires
to defrost the probe tip. Therefore, the instrument is exposed to
full bottle pressure only intermittently and for short periods of
time, greatly increasing the safety of the apparatus.
It is believed that the construction and operation of this
invention will now be apparent to those skilled in the art. It will
also be apparent that a number of variations and modifications may
be made in this invention without departing from its spirit and
scope. Accordingly, the foregoing description is to be construed as
illustrative only, rather than limiting. This invention is limited
only by the scope of the following claims.
* * * * *