US3688770A - High pressure gas pressurization system - Google Patents
High pressure gas pressurization system Download PDFInfo
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- US3688770A US3688770A US79183A US3688770DA US3688770A US 3688770 A US3688770 A US 3688770A US 79183 A US79183 A US 79183A US 3688770D A US3688770D A US 3688770DA US 3688770 A US3688770 A US 3688770A
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- chamber
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- high pressure
- conduits
- pressure reducing
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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61G—TRANSPORT, PERSONAL CONVEYANCES, OR ACCOMMODATION SPECIALLY ADAPTED FOR PATIENTS OR DISABLED PERSONS; OPERATING TABLES OR CHAIRS; CHAIRS FOR DENTISTRY; FUNERAL DEVICES
- A61G10/00—Treatment rooms or enclosures for medical purposes
- A61G10/02—Treatment rooms or enclosures for medical purposes with artificial climate; with means to maintain a desired pressure, e.g. for germ-free rooms
- A61G10/023—Rooms for the treatment of patients at over- or under-pressure or at a variable pressure
- A61G10/026—Rooms for the treatment of patients at over- or under-pressure or at a variable pressure for hyperbaric oxygen therapy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63C—LAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
- B63C11/00—Equipment for dwelling or working underwater; Means for searching for underwater objects
- B63C11/02—Divers' equipment
- B63C11/32—Decompression arrangements; Exercise equipment
Definitions
- I-Iyperbaric chambers that is, chambers which are operated at greater than atmospheric pressure, are utilized in a variety of fields including the medical field and diving field.
- the internal pressure of the hyperbaric chamber is increased to a desired value by the admission of a compressed gas.
- the compressed gas may be in the form of air, or oxygen combined with an inert gas such as helium or hydrogen.
- High pressure gas from a source is generally reduced to an intermediate pressure by means of a pressure regulator and is thereafter admitted into the hyperbaric chamber through a throttling valve. As more and more gas is admitted to the chamber to attain the desired pressure there is noticeable increase in temperature due to the heat of compression which occurs inside the chamber. Recorded incidents of l35to 140 F. temperatures have caused the halt of fast pressurization for occupant safety and the occupants have been known to resort to holding a wet cloth over their mouth to prevent breathing hot gas.
- the increase in temperature to these undesirable values often has a detrimental effect.
- a gas pressurization system which includes a hyperbaric chamber and a source of high pressure gas for pressurizing the chamber.
- High pressure conduit means connects the source and the high pressure gas with the inside of the chamber and pressure reducer means are connected with the conduit inside the chamber such that expansion of the high pressure gas takes place within the chamber.
- the pressure reducer means takes the form of a plurality of different size orifices selectively connectable with the high pressure conduit means, to provide for variable rates of pressurization.
- FIGS. 1 and 2 illustrate prior art gas pressurization systems
- FIG. 3 is a sketch illustrating the preferred embodiment of the present invention.
- FIGS. 4 and 5 illustrate different sized orifices which may be utilized on the ends of the conduits within the chamber of FIG. 3;
- FIGS. 6, 7 and 8 illustrate conduit terminations within the chamber of FIG. 3, for promoting better heat transfer.
- FIG. 1 there is illustrated a prior art system including a hyperbaric chamber 10, and for clarity, various instrumentation, life support equipment and entrances have been omitted.
- a hyperbaric chamber 10 find wide application in the medical field for performing research and medical operations, as well as the diving field for performing experiments at simulated ocean depths or as living quarters for divers who transfer into the chamber from a working depth in the water by means of a transfer chamber or capsule.
- the chamber 10 is connected with a source 12 of high pressure gas which includes a compressor 14 and a high pressure reservoir 15 which may be comprised of a large number of high pressure cylinders connected to the compressor 14 by means of adequate piping 17.
- the output at A of the high pressure reservoir 15 s generally thousands of pounds per square inch (psi) and this high pressure is reduced by means of pressure regulator 20 to an intermediate pressure of hundreds of psi, at point B.
- the conduit means 22 from the pressure regulator 20 feeds into the chamber 10 through a control or throttling valve 24 which is turned off when the gauge 26 reads the desired pressure.
- frost is often seen on the conduit and throttling valve while the temperature within the chamber rises to an uncomfortable level.
- FIG. 2 illustrates another prior art gas pressurization system and includes a compressor 30 connected to the chamber 10 by conduit means 32.
- the connection is made by way of a storage or volume tank 34 and a throttling valve 36 which is closed when the gauge 26 displays the desired chamber pressure.
- the arrangement of F 16.2 is somewhat different from the arrangement of FIG. 1 in that the compressor 30 supplying the volume tank 34 is of a relatively higher volumetric flowrate than compressor 14.
- the pressure at point C IS high relative to the ambient pressure but is generally lower than, for example, a much higher pressure at point A in FIG. 1.
- FIG. 2 illustrates a typical diffuser 38 having a plurality of holes 39. Where relatively fast descent rates are desired, the arrangement of FIG. 2 suffers the same deficiencies as the arrangement of FIG. 1.
- FIG. 3 there is illustrated one embodiment of the present invention, which includes a chamber 10 to be pressurized to a certain value indicatable by the gauge 26.
- the chamber 10 is connected by conduit means 43 to a source of high pressure gas 45 which for purposes of illustration may include compressor and high pressure reservoir as illustrated in FIG. 1.
- the conduit means 43 includes conduit 48 connected to, or which branches into a plurality of conduits 50 to 54 which enter the chamber 10.
- the conduits 50 to 54 have respective valving means 60 to 64 in line therewith and preferably being of the type which operate in two positions, one being fully closed and the other being fully opened.
- a similar valves 65 is located in conduit 48 to allow or to block the passage of high pressure gas into the parallel branches.
- One type of valve which accomplishes this function is a motor operated ball valve and in order to control the opening and closing of the valves 60 to 65 from a remote position there is provided a control panel 68 whereby an operator may provide individual signals to open or close selected valves.
- the ends 70 to 74 of the respective conduits 50 to 54 are disposed within the chamber 10 and include pressure reducer, or flow restriction means whereby the high pressure gas from the source 45 is discharged directly into the chamber through the pressure reducer means and the consequent expansion of the high pressure gas within the chamber effects cooling thereof, similar to the expansion of a gas in a refrigerator cooling cycle.
- the rate of pressurization of the chamber 10 for a particular gas is dependent upon the mass flow rate of the gas into the chamber, which in turn is governed by selective operation of valves 60 to 64.
- FIG. 4 illustrates, in more detail, the ends 70 to 74 of the conduits within the chamber 10 of FIG. 3.
- Each conduit within the chamber has associated therewith a pressure reducer means such as orifice plates 80 to 84.
- Each orifice plate 80 to 84 has a respective pressure reducing aperture and if all apertures were of the same size, then by selective energization of ball valves 60 to 64, five different pressurization rates could be selected.
- the number of different pressurization rates is more than doubled in the present invention by the provision of different sized orifices, each having an area A 2"( C), wherein n is a whole number between zero and the number of conduits minus 1, and C is a constant.
- ball valves 60 to 64 31 possible pressurization rates may be provided.
- FIG. 5 illustrates orifice plates 80' to 84' each having an efiective total aperture area equal to its counterpart of FIG. 4. This is accomplished by making an aperture of a certain diameter, for example, by drilling, in orifice plate 80', drilling two of those same diameter apertures in plate 81', four of those same diameter apertures in plate 82', eight in plate 83, and 16 in plate 84'.
- the apertures are relatively small to accomplish the pressure reducing gas expansion function.
- the orifice size varies with the size of chamber, desired rate of pressurization, the input pressure and the density of the gas utilized. By way of example for air at a pressure of 3,000 psi pressurizing a chamber of approximately 500 cu. ft. at a simulated descent rate of 6 ft. per minute, ball valve 60 (and 65) would be opened and the aperture within the chamber would have a diameter of 0.025 inches.
- FIG. 6 illustrates one such arrangement.
- Conduit 90 is disposed within the chamber to be pressurized, and includes a plurality of pressure reducing apertures 92 which may be drilled into the conduit 90 and arranged along the length thereof to also act as a diffuser for better gas mixing.
- the remaining conduits within the chamber may have a greater or lesser number of apertures such that the total effective aperture area is in-accordance with the previously given equation.
- Connected to the conduit and disposed between adjacent apertures 92 are a plurality of heat exchanger means in the form of fins 94 providing a relatively large surface area for heat exchange purposes.
- FIG. 7 is illustrative of another type of heat exchanger arrangement which may be utilized.
- Conduit 96 is a gas discharge conduit located within the chamber and includes a plurality of stubs or projections 98 having at the ends thereof a pressure reducer aperture. Disposed about each aperture is venturi tube 100 having a converging and diverging portion. When high pressure gas is discharged through the apertures in the stubs 98, chamber gas is caused to flow through the venturi tubes, as indicated by the arrows, to thereby promote gas flow for additional heat transfer, fins could be provided axially within the venturi tube 100 and mixing within the chamber.
- conduit 103 is disposed within'the chamber and includes at the end thereof a high pressure swivel 105.
- a high pressure swivel 105 Connected to the high pressure swivel is a plurality of blades or vanes 108 each having respective channel 110 therein connecting the conduit 103 with respective discharge orifices 112. Gas discharge through these orifices 1 12 causes the blades 108 to turn to thereby stir up the chamber gas to promote mixing thereof.
- a gas pressurization system comprising:
- means including conduit means connecting said source with the inside of said chamber for delivering said gas to said chamber at substantially said same high pressure;
- relatively small aperture means connected with said conduit means within said chamber and being of such size that rapid expansion of said high pressure gas discharging through said relatively small aperture means provides cooling of said gas.
- said conduit means includes a plurality of conduits each having pressure reducing orifice means within said chamber.
- a system according to claim 2 which includes:
- valves are of the type which are either fully opened or fully closed.
- said plurality of conduits have respectively different sized pressure reducing orifices.
- At least two of said conduits include a plurality of similar sized pressure reducing orifices, with the second of said two having a greater number of said pressure reducing orifices.
- At least one of said conduits includes a plurality of pressure reducing orifices disposed along the length thereof and which additionally includes b. a heat exchanger means disposed along the length of said conduit.
- said heat exchanger means comprises a plurality of 10 from a high pressure gas source comprising the steps of:
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Abstract
High pressure gas is fed into a hyperbaric chamber to be pressurized, directly through a series of pressure reducing orifices. The expansion of the high pressure gas that results, effects a cooling of the interior of the chamber.
Description
United States Patent ONeill Sept. 5, 1972 54] HIGH PRESSURE GAS 56 References Cited PRESSURIZATION SYSTEM UNITED STATES PATENTS Inventor: Wilbur L P M 1,224,180 5 1917 Lake" ..128/204 73 A 1 Ekctdc C 6 1,842,710 1/1932 Besehf ..62/87X 1 3 g 3,188,824 6/1965 Geisteta] ..62/86 3,271,970 9/1966 Berner ..62/87 x 22 Filed: Oct. 8, 1970 3,387,580 6/1968 Walker ..6l/69RX [211 App] 79 183 "3,509,810 5/1970 Riester ..98/1.5
Primary Examiner-Albert W. Davis, Jr. 52 U.S.CI. ..128/204,61/69 R, 62/86, KliPfeland Schm" 62/401, 98/l.5
[51 InLCI. ..A6lm 16/00 [57] ABSTRACT [58] Field of Search ..62/86, 87, 78, 401; 137/14, High pressure gas is fed into a hyperbaric chamber 16 be pressurized, directly through a series of pressure reducing orifices. The expansion of the high pressure gas that results, efiects a cooling of the interior of the chamber.
' l2Claims,8DrawingFigures I x i HIGH PRESSURE GAS HIGH PRESSURE GAS PRESSURIZATION SYSTEM BACKGROUND OF THE INVENTION 1. Field of the Invention I-Iyperbaric chamber complexes.
2. Description of the Prior Art I-Iyperbaric chambers, that is, chambers which are operated at greater than atmospheric pressure, are utilized in a variety of fields including the medical field and diving field. In operation, the internal pressure of the hyperbaric chamber is increased to a desired value by the admission of a compressed gas. For large chambers housing personnel the compressed gas may be in the form of air, or oxygen combined with an inert gas such as helium or hydrogen.
High pressure gas from a source is generally reduced to an intermediate pressure by means of a pressure regulator and is thereafter admitted into the hyperbaric chamber through a throttling valve. As more and more gas is admitted to the chamber to attain the desired pressure there is noticeable increase in temperature due to the heat of compression which occurs inside the chamber. Recorded incidents of l35to 140 F. temperatures have caused the halt of fast pressurization for occupant safety and the occupants have been known to resort to holding a wet cloth over their mouth to prevent breathing hot gas.
Where the chamber additionally includes temperature sensitive instruments or equipment, the increase in temperature to these undesirable values often has a detrimental effect.
SUMMARY OF THE INVENTION A gas pressurization system is provided which includes a hyperbaric chamber and a source of high pressure gas for pressurizing the chamber. High pressure conduit means connects the source and the high pressure gas with the inside of the chamber and pressure reducer means are connected with the conduit inside the chamber such that expansion of the high pressure gas takes place within the chamber.
The pressure reducer means takes the form of a plurality of different size orifices selectively connectable with the high pressure conduit means, to provide for variable rates of pressurization.
BRIEF DESCRIPTION OF THE DRAWINGS FIGS. 1 and 2 illustrate prior art gas pressurization systems;
FIG. 3 is a sketch illustrating the preferred embodiment of the present invention; I
FIGS. 4 and 5 illustrate different sized orifices which may be utilized on the ends of the conduits within the chamber of FIG. 3; and
FIGS. 6, 7 and 8 illustrate conduit terminations within the chamber of FIG. 3, for promoting better heat transfer.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring to FIG. 1, there is illustrated a prior art system including a hyperbaric chamber 10, and for clarity, various instrumentation, life support equipment and entrances have been omitted. Such chambers find wide application in the medical field for performing research and medical operations, as well as the diving field for performing experiments at simulated ocean depths or as living quarters for divers who transfer into the chamber from a working depth in the water by means of a transfer chamber or capsule.
The chamber 10 is connected with a source 12 of high pressure gas which includes a compressor 14 and a high pressure reservoir 15 which may be comprised of a large number of high pressure cylinders connected to the compressor 14 by means of adequate piping 17.
The output at A of the high pressure reservoir 15 s generally thousands of pounds per square inch (psi) and this high pressure is reduced by means of pressure regulator 20 to an intermediate pressure of hundreds of psi, at point B. The conduit means 22 from the pressure regulator 20 feeds into the chamber 10 through a control or throttling valve 24 which is turned off when the gauge 26 reads the desired pressure.
Depending upon the rate of descent, or rate of pressurization, frost is often seen on the conduit and throttling valve while the temperature within the chamber rises to an uncomfortable level.
FIG. 2 illustrates another prior art gas pressurization system and includes a compressor 30 connected to the chamber 10 by conduit means 32. The connection is made by way of a storage or volume tank 34 and a throttling valve 36 which is closed when the gauge 26 displays the desired chamber pressure. The arrangement of F 16.2 is somewhat different from the arrangement of FIG. 1 in that the compressor 30 supplying the volume tank 34 is of a relatively higher volumetric flowrate than compressor 14. The pressure at point C IS high relative to the ambient pressure but is generally lower than, for example, a much higher pressure at point A in FIG. 1.
In order to insure for better mixing of the gas as it enters the chamber 10, some systems include a diffuser at the end of the conduit and within the chamber for breaking up the gas stream into a plurality of gas streams. FIG. 2 illustrates a typical diffuser 38 having a plurality of holes 39. Where relatively fast descent rates are desired, the arrangement of FIG. 2 suffers the same deficiencies as the arrangement of FIG. 1.
In FIG. 3, there is illustrated one embodiment of the present invention, which includes a chamber 10 to be pressurized to a certain value indicatable by the gauge 26. The chamber 10 is connected by conduit means 43 to a source of high pressure gas 45 which for purposes of illustration may include compressor and high pressure reservoir as illustrated in FIG. 1.
The conduit means 43 includes conduit 48 connected to, or which branches into a plurality of conduits 50 to 54 which enter the chamber 10.
The conduits 50 to 54 have respective valving means 60 to 64 in line therewith and preferably being of the type which operate in two positions, one being fully closed and the other being fully opened. A similar valves 65 is located in conduit 48 to allow or to block the passage of high pressure gas into the parallel branches. One type of valve which accomplishes this function is a motor operated ball valve and in order to control the opening and closing of the valves 60 to 65 from a remote position there is provided a control panel 68 whereby an operator may provide individual signals to open or close selected valves.
The ends 70 to 74 of the respective conduits 50 to 54 are disposed within the chamber 10 and include pressure reducer, or flow restriction means whereby the high pressure gas from the source 45 is discharged directly into the chamber through the pressure reducer means and the consequent expansion of the high pressure gas within the chamber effects cooling thereof, similar to the expansion of a gas in a refrigerator cooling cycle.
The rate of pressurization of the chamber 10 for a particular gas is dependent upon the mass flow rate of the gas into the chamber, which in turn is governed by selective operation of valves 60 to 64.
Additional reference should now be made to FIG. 4 which illustrates, in more detail, the ends 70 to 74 of the conduits within the chamber 10 of FIG. 3. Each conduit within the chamber has associated therewith a pressure reducer means such as orifice plates 80 to 84. Each orifice plate 80 to 84 has a respective pressure reducing aperture and if all apertures were of the same size, then by selective energization of ball valves 60 to 64, five different pressurization rates could be selected. The number of different pressurization rates is more than doubled in the present invention by the provision of different sized orifices, each having an area A 2"( C), wherein n is a whole number between zero and the number of conduits minus 1, and C is a constant. For
example, in FIG. 4 if orifice plate 84 is the fourth (n=4) orifice plate 83 is the third (n=3), orifice plate 82 is the second (n=2) orifice plate is the first (n=l), and orifice plate 80 is the zero (n=), and arbitrarily making C equal to 1, then the area of each orifice or aperture, is as follows: for plate 80, A=1; for plate 81, A=2; for plate 82, A=4; for plate 83, A=8; and for plate 84 A=l6. By selective choice of ball valves 60 to 64, 31 possible pressurization rates may be provided.
FIG. 5 illustrates orifice plates 80' to 84' each having an efiective total aperture area equal to its counterpart of FIG. 4. This is accomplished by making an aperture of a certain diameter, for example, by drilling, in orifice plate 80', drilling two of those same diameter apertures in plate 81', four of those same diameter apertures in plate 82', eight in plate 83, and 16 in plate 84'. The apertures are relatively small to accomplish the pressure reducing gas expansion function. The orifice size varies with the size of chamber, desired rate of pressurization, the input pressure and the density of the gas utilized. By way of example for air at a pressure of 3,000 psi pressurizing a chamber of approximately 500 cu. ft. at a simulated descent rate of 6 ft. per minute, ball valve 60 (and 65) would be opened and the aperture within the chamber would have a diameter of 0.025 inches.
Due to the expansion of high pressure gas into the chamber with the consequent cooling, there may be a tendency for the orifice plates 80 to 84, or 80' to 84', to frost up. Accordingly, in accordance with the preferred embodiment of the present invention a heat exchange arrangement is provided for the conduit means within the chamber. FIG. 6 illustrates one such arrangement. Conduit 90 is disposed within the chamber to be pressurized, and includes a plurality of pressure reducing apertures 92 which may be drilled into the conduit 90 and arranged along the length thereof to also act as a diffuser for better gas mixing. The remaining conduits within the chamber may have a greater or lesser number of apertures such that the total effective aperture area is in-accordance with the previously given equation. Connected to the conduit and disposed between adjacent apertures 92 are a plurality of heat exchanger means in the form of fins 94 providing a relatively large surface area for heat exchange purposes.
FIG. 7 is illustrative of another type of heat exchanger arrangement which may be utilized. Conduit 96 is a gas discharge conduit located within the chamber and includes a plurality of stubs or projections 98 having at the ends thereof a pressure reducer aperture. Disposed about each aperture is venturi tube 100 having a converging and diverging portion. When high pressure gas is discharged through the apertures in the stubs 98, chamber gas is caused to flow through the venturi tubes, as indicated by the arrows, to thereby promote gas flow for additional heat transfer, fins could be provided axially within the venturi tube 100 and mixing within the chamber.
Another gas mixing arrangement is illustrated in FIG. 8 wherein conduit 103 is disposed within'the chamber and includes at the end thereof a high pressure swivel 105. Connected to the high pressure swivel is a plurality of blades or vanes 108 each having respective channel 110 therein connecting the conduit 103 with respective discharge orifices 112. Gas discharge through these orifices 1 12 causes the blades 108 to turn to thereby stir up the chamber gas to promote mixing thereof.
I claim as my invention:
1. A gas pressurization system comprising:
a. a hyperbaric chamber;
b. a source of relatively high pressure gas for pressurizing said chamber;
c. means including conduit means connecting said source with the inside of said chamber for delivering said gas to said chamber at substantially said same high pressure; and
d. relatively small aperture means connected with said conduit means within said chamber and being of such size that rapid expansion of said high pressure gas discharging through said relatively small aperture means provides cooling of said gas.
2. A system according to claim 1 wherein:
a. said conduit means includes a plurality of conduits each having pressure reducing orifice means within said chamber.
3. A system according to claim 2 which includes:
a. a plurality of valves, each for controlling gas flow in a respective one of said plurality of conduits.
4. A system according to claim 3 wherein:
a. said valves are of the type which are either fully opened or fully closed.
5. A system according to claim 2 wherein:
a. said plurality of conduits have respectively different sized pressure reducing orifices.
6. A system according to claim 5 wherein:
' a. each said pressure reducing orifice has an area A=2"(c), where c is a constant and n is a particular conduit number between zero and the total number of conduits minus 1.
7. A system according to claim 2 wherein:
a. at least two of said conduits include a plurality of similar sized pressure reducing orifices, with the second of said two having a greater number of said pressure reducing orifices.
8. A system according to claim 7 wherein:
a. the total effective orifice area of said plurality of pressure reducing orifices is A=2"(c), where c is a constant and n is a particular conduit number between zero and the total number of conduits minus 1.
9. A system according to claim 2 wherein:
a. at least one of said conduits includes a plurality of pressure reducing orifices disposed along the length thereof and which additionally includes b. a heat exchanger means disposed along the length of said conduit.
10. A system according to claim 9 wherein:
a. said heat exchanger means comprises a plurality of 10 from a high pressure gas source comprising the steps of:
a. discharging said high pressure gas directly into said chamber through at least one pressure reducing orifice of such a size that the rapid expansion of said high pressure gas discharging therethrough provides cooling of said gas; and
b. shutting off said discharge when a desired chamber pressure is attained.
Claims (12)
1. A gas pressurization system comprising: a. a hyperbaric chamber; b. a source of relatively high pressure gas for pressurizing said chamber; c. means including conduit means connecting said source with the inside of said chamber for delivering said gas to said chamber at substantially said same high pressure; and d. relatively small aperture means connected with said conduit means within said chamber and being of such size that rapid expansion of said high pressure gas discharging through said relatively small aperture means provides cooling of said gas.
2. A system according to claim 1 wherein: a. said conduit means includes a plurality of conduits each having pressure reducing orifice means within said chamber.
3. A system according to claim 2 which includes: a. a plurality of valves, each for controlling gas flow in a respective one of said plurality of conduits.
4. A system according to claim 3 wherein: a. said valves are of the type which are either fully opened or fully closed.
5. A system according to claim 2 wherein: a. said plurality of conduits have respectively different sized pressure reducing orifices.
6. A system according to claim 5 wherein: a. each said pressure reducing orifice has an area A 2n(c), where c is a constant and n is a particular conduit number between zero and the total number of conduits minus 1.
7. A system according to claim 2 wherein: a. at least two of said conduits include a plurality of similar sized pressure reducing orifices, with the second of said two having a greater number of said pressure reducing orifices.
8. A system according to claim 7 wherein: a. the total effective orifice area of said plurality of pressure reducing orifices is A 2n(c), where c is a constant and n is a particular conduit number between zero and the total number of conduits minus 1.
9. A system according to claim 2 wherein: a. at least one of said conduits includes a plurality of pressure reducing orifices disposed along the length thereof and which additionally includes b. a heat exchanger means disposed along the length of said conduit.
10. A system according to claim 9 wherein: a. said heat exchanger means comprises a plurality of fins disposed between adjacent pressure reducing orifices.
11. A system according to claim 2 wherein: a. at least one of said conduits includes a plurality of projections each having pressure reducing orifice means, and which additionally includes b. a plurality of venturi tubes, each disposed over a respective one of said projections.
12. A method of pressurizing a hyperbaric chamber from a high pressure gas source comprising the steps of: a. discharging said high pressure gas directly into said chamber through at least one pressure reducing orifice of such a size that the rapid expansion of said high pressure gas discharging therethrough provides cooling of said gas; and b. shutting off said discharge when a desired chamber pressure is attained.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US7918370A | 1970-10-08 | 1970-10-08 |
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US3688770A true US3688770A (en) | 1972-09-05 |
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US79183A Expired - Lifetime US3688770A (en) | 1970-10-08 | 1970-10-08 | High pressure gas pressurization system |
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AU (1) | AU465169B2 (en) |
BE (1) | BE773646A (en) |
CA (1) | CA940724A (en) |
DE (1) | DE2149372A1 (en) |
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FR2493699A1 (en) * | 1980-11-12 | 1982-05-14 | Bel Hamri Bernard | Room for heat treatment of patient - includes infra-red source for raising patient's internal temp. after blood transfusion |
US4362154A (en) * | 1979-03-21 | 1982-12-07 | Laboratories De Mecaniques Appliquees "Lama" | Processes and devices for regulating the oxygen partial pressure of the gas mixture of the respiratory circuit of a diver |
US4642997A (en) * | 1984-03-31 | 1987-02-17 | Deutsche Airbus Gmbh | Process and apparatus for power-and air conditioning-fresh air generation in aircraft |
US5423313A (en) * | 1981-03-10 | 1995-06-13 | Siemens-Elema Ab | Respirator intended for connection to human or animal airways |
US5713212A (en) * | 1997-02-07 | 1998-02-03 | Mcdonnell Douglas Corporation | Apparatus and method for generating air stream |
US5908402A (en) * | 1997-02-03 | 1999-06-01 | Valleylab | Method and apparatus for detecting tube occlusion in argon electrosurgery system |
US6283123B1 (en) | 1994-12-01 | 2001-09-04 | Keith W. Van Meter | Hyperbaric resuscitation system and method |
US20080028774A1 (en) * | 2006-08-03 | 2008-02-07 | Machflow Energy, Inc. | Rare-gas-based Bernoulli heat pump and method |
US20090145155A1 (en) * | 2004-06-18 | 2009-06-11 | Williams Arthur R | Rotating Bernoulli Heat Pump |
US20090177569A1 (en) * | 2008-01-03 | 2009-07-09 | Bowers Jeffrey A | Water alteration structure risk management or ecological alteration management systems and methods |
US20090173801A1 (en) * | 2008-01-03 | 2009-07-09 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Water alteration structure and system having below surface valves or wave reflectors |
US20090175685A1 (en) * | 2008-01-03 | 2009-07-09 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Water alteration structure movement method and system |
US20090183858A1 (en) * | 2005-06-24 | 2009-07-23 | Williams Arthur R | Venturi for Heat Transfer |
US20090277192A1 (en) * | 2005-03-09 | 2009-11-12 | Williams Arthur R | Centrifugal bernoulli heat pump |
US20100300560A1 (en) * | 2008-01-03 | 2010-12-02 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Water alteration structure and system having heat transfer conduit |
WO2015040614A1 (en) * | 2013-09-18 | 2015-03-26 | Inhaletech Llc | Body core temperature cooling device |
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US3188824A (en) * | 1962-04-05 | 1965-06-15 | Air Prod & Chem | Refrigeration method and apparatus employing the joule-thomson effect |
US3271970A (en) * | 1962-10-29 | 1966-09-13 | Pennsylvania Wmb Inc | Insulated cold storage rooms or similar enclosures |
US3387580A (en) * | 1965-10-22 | 1968-06-11 | Harold H. Walker | Submersible water craft |
US3509810A (en) * | 1965-11-04 | 1970-05-05 | Daimler Benz Ag | Motor vehicle with protection installation against contamination of interior space by means of abc-war materials |
-
1970
- 1970-10-08 US US79183A patent/US3688770A/en not_active Expired - Lifetime
-
1971
- 1971-07-26 ZA ZA714979A patent/ZA714979B/en unknown
- 1971-07-28 AU AU31728/71A patent/AU465169B2/en not_active Expired
- 1971-08-05 GB GB3676771A patent/GB1337152A/en not_active Expired
- 1971-08-27 CA CA121,514A patent/CA940724A/en not_active Expired
- 1971-10-02 DE DE19712149372 patent/DE2149372A1/en active Pending
- 1971-10-07 FR FR7136088A patent/FR2111095A5/fr not_active Expired
- 1971-10-08 BE BE773646A patent/BE773646A/en unknown
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US1224180A (en) * | 1913-06-06 | 1917-05-01 | Simon Lake | Apparatus for treating certain diseases of the human body. |
US1842710A (en) * | 1925-02-23 | 1932-01-26 | Zeppelin Luftschiffbau | Device for drying lifting gas for airships |
US3188824A (en) * | 1962-04-05 | 1965-06-15 | Air Prod & Chem | Refrigeration method and apparatus employing the joule-thomson effect |
US3271970A (en) * | 1962-10-29 | 1966-09-13 | Pennsylvania Wmb Inc | Insulated cold storage rooms or similar enclosures |
US3387580A (en) * | 1965-10-22 | 1968-06-11 | Harold H. Walker | Submersible water craft |
US3509810A (en) * | 1965-11-04 | 1970-05-05 | Daimler Benz Ag | Motor vehicle with protection installation against contamination of interior space by means of abc-war materials |
Cited By (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4362154A (en) * | 1979-03-21 | 1982-12-07 | Laboratories De Mecaniques Appliquees "Lama" | Processes and devices for regulating the oxygen partial pressure of the gas mixture of the respiratory circuit of a diver |
FR2493699A1 (en) * | 1980-11-12 | 1982-05-14 | Bel Hamri Bernard | Room for heat treatment of patient - includes infra-red source for raising patient's internal temp. after blood transfusion |
US5423313A (en) * | 1981-03-10 | 1995-06-13 | Siemens-Elema Ab | Respirator intended for connection to human or animal airways |
US4642997A (en) * | 1984-03-31 | 1987-02-17 | Deutsche Airbus Gmbh | Process and apparatus for power-and air conditioning-fresh air generation in aircraft |
US6283123B1 (en) | 1994-12-01 | 2001-09-04 | Keith W. Van Meter | Hyperbaric resuscitation system and method |
US6139519A (en) * | 1997-02-03 | 2000-10-31 | Sherwood Services Ag | Method and apparatus for detecting tube occlusion |
US5908402A (en) * | 1997-02-03 | 1999-06-01 | Valleylab | Method and apparatus for detecting tube occlusion in argon electrosurgery system |
US5713212A (en) * | 1997-02-07 | 1998-02-03 | Mcdonnell Douglas Corporation | Apparatus and method for generating air stream |
US20090145155A1 (en) * | 2004-06-18 | 2009-06-11 | Williams Arthur R | Rotating Bernoulli Heat Pump |
US7823405B2 (en) | 2004-06-18 | 2010-11-02 | Williams Arthur R | Rotating bernoulli heat pump |
US7918094B2 (en) | 2005-03-09 | 2011-04-05 | Machflow Energy, Inc. | Centrifugal bernoulli heat pump |
US20090277192A1 (en) * | 2005-03-09 | 2009-11-12 | Williams Arthur R | Centrifugal bernoulli heat pump |
US20090183858A1 (en) * | 2005-06-24 | 2009-07-23 | Williams Arthur R | Venturi for Heat Transfer |
US20080028774A1 (en) * | 2006-08-03 | 2008-02-07 | Machflow Energy, Inc. | Rare-gas-based Bernoulli heat pump and method |
US7908872B2 (en) * | 2006-08-03 | 2011-03-22 | Machflow Energy Inc. | Rare-gas-based bernoulli heat pump and method |
US20090173404A1 (en) * | 2008-01-03 | 2009-07-09 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Water alteration structure and system |
US20090175685A1 (en) * | 2008-01-03 | 2009-07-09 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Water alteration structure movement method and system |
US20090173386A1 (en) * | 2008-01-03 | 2009-07-09 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Water alteration structure applications and methods |
US20100300560A1 (en) * | 2008-01-03 | 2010-12-02 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Water alteration structure and system having heat transfer conduit |
US20090173801A1 (en) * | 2008-01-03 | 2009-07-09 | Searete Llc, A Limited Liability Corporation Of The State Of Delaware | Water alteration structure and system having below surface valves or wave reflectors |
US20090177569A1 (en) * | 2008-01-03 | 2009-07-09 | Bowers Jeffrey A | Water alteration structure risk management or ecological alteration management systems and methods |
US8348550B2 (en) * | 2008-01-03 | 2013-01-08 | The Invention Science Fund I Llc | Water alteration structure and system having heat transfer conduit |
US8679331B2 (en) | 2008-01-03 | 2014-03-25 | The Invention Science Fund I Llc | Water alteration structure movement method and system |
US8685254B2 (en) | 2008-01-03 | 2014-04-01 | The Invention Science Fund I Llc | Water alteration structure applications and methods |
US8702982B2 (en) | 2008-01-03 | 2014-04-22 | The Invention Science Fund I Llc | Water alteration structure and system |
US8715496B2 (en) | 2008-01-03 | 2014-05-06 | The Invention Science Fund I Llc | Water alteration structure and system having below surface valves or wave reflectors |
WO2015040614A1 (en) * | 2013-09-18 | 2015-03-26 | Inhaletech Llc | Body core temperature cooling device |
US10434275B2 (en) | 2013-09-18 | 2019-10-08 | Inhaletech Llc | Body core temperature cooling device |
Also Published As
Publication number | Publication date |
---|---|
DE2149372A1 (en) | 1972-08-10 |
CA940724A (en) | 1974-01-29 |
GB1337152A (en) | 1973-11-14 |
BE773646A (en) | 1972-04-10 |
AU3172871A (en) | 1973-02-01 |
FR2111095A5 (en) | 1972-06-02 |
ZA714979B (en) | 1972-04-26 |
AU465169B2 (en) | 1975-09-18 |
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