US3107988A - Liquid vapor separator - Google Patents
Liquid vapor separator Download PDFInfo
- Publication number
- US3107988A US3107988A US55339A US5533960A US3107988A US 3107988 A US3107988 A US 3107988A US 55339 A US55339 A US 55339A US 5533960 A US5533960 A US 5533960A US 3107988 A US3107988 A US 3107988A
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- Prior art keywords
- tank
- liquid
- gas
- centrifuge
- vent
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- 239000007788 liquid Substances 0.000 title claims description 45
- 239000000203 mixture Substances 0.000 claims description 15
- 230000000903 blocking effect Effects 0.000 claims description 10
- 239000007789 gas Substances 0.000 description 40
- 230000007246 mechanism Effects 0.000 description 10
- 239000012530 fluid Substances 0.000 description 9
- 239000002245 particle Substances 0.000 description 6
- 230000001105 regulatory effect Effects 0.000 description 6
- 230000005484 gravity Effects 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 3
- 239000008241 heterogeneous mixture Substances 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 239000004078 cryogenic material Substances 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 238000013022 venting Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 235000020061 kirsch Nutrition 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/008—Details of vessels or of the filling or discharging of vessels for use under microgravity conditions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B04—CENTRIFUGAL APPARATUS OR MACHINES FOR CARRYING-OUT PHYSICAL OR CHEMICAL PROCESSES
- B04B—CENTRIFUGES
- B04B5/00—Other centrifuges
- B04B5/10—Centrifuges combined with other apparatus, e.g. electrostatic separators; Sets or systems of several centrifuges
Definitions
- a receptacle containing a volatile cryogenic material such as liquid hydrogen
- a receptacle may be subject to radiant heat from the sun or other heat source which will tend to heat the liquid and change some portions of the liquid to the vapor state with a consequent increase in the pressure in the receptacle.
- a vent located anywhere in the tank would vent both vapor and liquid indiscriminately and mechanism supported anywhere in the tank would, under those conditions, be submerged in the mixture.
- An object of this invention is to provide vent control mechanism which will select the vapor as the material to be vented from a pressurized container of a heterogeneous mixture of vapor and liquid, and retain the liquid.
- FIGURE 1 is a schematic showing of the vent and separator installed in a receptacle.
- FIGURE 2 is a sectional view of the vent motor and separator.
- FIGURE 3 is a plan view of the motor showing the pressure regulating valve and control.
- FIGURE 4 is a sectional view on line 4-4 of FIG- URE 5 of a modified form of motor, separator, and relief valve, installed in a receptacle with the outlet valve removed.
- FIGURE 5 is a front elevation showing the connections to the heat exchanger and the control valve.
- FIGURE 6 is a sectional view of the control valve.
- FIGURES 1 to 3 essentially consi-sts of a centrifugal separator indicated generally at 10 powered by a positive displacement motor 12. and a pressure regulating and shut-off valve 14.
- This mechanism is all arranged in a tank vent 16.
- the vent separator is composed of an axial fiow fan 18 for establishing the centrifugal field in separating the liquid and gas.
- a diffuser 20 is provided for reducing the velocity of the fluid flow returning to the tank.
- the gas separated by the centrifugal field created by the fan 18 is used to power the positive displacement gear motor 12 and is then vented overboard through the pressure regulating valve 14. All leakage paths through the vent separator have been located upstream of the valve 14 so that the valve leakge will be the only leakage from the system.
- FIGS. 4, 5, and 6 while broadly similar to the device shown in FIGS. 1-3 consists of a centrifugal separator indicated generally at 10, powered by a simple reaction turbine 22, a tube-type heat exchanger 24, a pressure regulating valve, and a solenoid operated shut-01f valve 28 all, a-s-shown in FIGS. 4, 5 and 6, supported in a receptacle from one of the walls 32 of the receptacle by suitable means, such as bolts 31, and under zero gravity conditions submerged in the mixture in the receptacle.
- the separator is composed of an axial flow fan for establishing the centrifugal field and in separating the liquid and gas.
- the gas to be vented is separated by the fan and passed through the direct acting, pressure regulator 26 located in the main housing 27 of the assembly before it enters the turbine 22. Because a temperature drop is experienced by the gas in passing through the turbine 22, and because some liquid droplets may be present, a heat exchanger 24 is incorporated to transfer heat from the mixture inside of the tank or receptacle to the cooled gas being vented.
- a shut-off valve 28 is provided down-stream of the heat exchanger 24 in the vented gas line. This valve 28 is solenoid-ac-tuated'and manually controlled to both the open and closed positions. A switch on the valve may be used to indicate the valve position.
- the tank or receptacle to be vented is indicated at 32, and the vent 16 connects the interior of the tank with the exterior thereof.
- the separator mechanism including the separator 10 and the motor 12 is located in the vent 16 and forms a part thereof.
- the vent and separator mechanism may be supported in the tank in any suitable manner such as on one of the tank walls or from any other suitable support.
- a duct 34 forming pant of the vent 16- is supported in the tank from the main body 36 of the separator and forms the outer casing for the fan 18 and may be partitioned from the remainder of the tank by a bafiie 37 if desired.
- Fan blades 38 are supported on a shaft 40 which is supported in bearings 42 and 44 and is directly connected with one of the gears 46 of the gear motor 12.
- the fan 18 is designed to impart a swirling motion to the fluid received in the duct 34 and assists the pressure difference between the inside and the outside of the tank in moving the fluid through the duct 34.
- the swirling motion will act as a centrifuge to drive the heavier or liquid particles toward the periphery of the duct, thus displacing the lighter or gaseous particles toward the fan shaft 40.
- the gas particles will be forced through the orifice 48 into the hollow interior 50 of the shaft 40, and will be vented through the orifice 5-2 to the annulus 54 and then through duct 56 to the gear motor or expansion device 12.
- the expansion device will be driven by these pressurized gases and drive the shaft 40 and the fan 18.
- the liquid particles centrifuged to the outside of the duct 34 together with excess gas which did not pass through orifice 48 will pass through the diffuser 2@ to efliciently change their velocity into static pressure and will then be discharged directly back into the portion of the tank surrounding the separator.
- the gas discharged from the motor 12 is led through the portions 60 of the vent 16 to the pnessure regulating and shut-off valve 14.
- the valve 14 comprises a springpressed valve member 62 blocking the passage 60 from the outlet passage '64 of the vent 16 leading overboard or to ambient.
- Plunger 62 in addition to being urged to closed position by spring 66 is also urged to closed position by fluid pressure acting on the surface 68 of the plunger 62.
- Fluid is led through line 71, from the passage 56 leading to the gear motor, into the chamber 70 to act on the surface 68.
- a restriction 72 limits the rate of flow of fluid to the chamber 70.
- Fluid may be vented to ambient, by connections not shown, from the chamber 70, faster than it is admitted past restriction 72, by the valve 74 controlled by pressure in the bellows 76 which is connected by conduit 78 with the tank 32.
- Bellows 8d the outside of which is connected, by connections not shown, with ambient, is balanced between springs 82 and 84 and as this device is intended to operate in the outer atmosphere where the pressure is substantially zero the pressure outside of the bellows is substantially zero.
- a valve 86 controlled by solenoid 88 is used to block the exit passage from the valve 74 and thus hold the valve 62 in closed position, when desired.
- FIGURES 4 to 6 The modification as shown in FIGURES 4 to 6 is broadly similar to that shown in FIGS. 1-3 and differs from that previously described mainly in the location of the pressure regulating valve between the separator and the turbine and the incorp-oraiton of a heat exchanger in the turbine exhaust. Also FIGURES 2 and 4 differ in the type of expansion device shown. FIGURE 2 shows positive displacement; FIGURE 4, a turbine. The actual configuration of expansion device used in any particular application is dependent on considerations such as cost and efficiency.
- the fan 30' having blades 38 supported on a shaft 40 is located similar to that shown in FIGS. 1-3 in a duct 34, a portion of which acts as a casing for the fan.
- the shaft 40 is supported in bearings 42.
- the fan 30 imparts a swirling motion to the mixture of gas and liquid received in the duct 34 and acts as a centrifuge toforce the liquid towards the outer periphery of the duct 34- and discharge it through the diffuser 20.
- a heat exchanger 24 is arranged around the outer periphery of the diffuser 2d and the liquid and excess gas discharged by the fan 30 passes through this heat exchanger, around the exterior of the heat exchanger tubes, on its Way back to the portion of the tank surrounding the separator Gas to be vented is separated from the mixture of gas and liquid by the centrifuge action of the fan and passes through the orifice 90 around the outside of shaft 40 and under the spring-pressed poppet valve 26, supported on evacuated bellows 92. After opening and passing the poppet valve 26, the gas passes through orifice 94 through the interior of the turbine rotor 22 to be discharged at its periphery.
- the discharged gas which is cooled due to expansion through the turbine and because of the work done in turning the fan is led through duct 96 to a chamber 97, partitioned off by a partition 99, in a manifold 131 and thence to the interior of the tubes of the heat exchanger 24.
- the discharged gas is led through a chamber 108 formed in the manifold 101 by the partition 99 and then through duct 98 to the shut-off valve 28.
- the heat exchanger may be located in duct 35 to cool the mixture before it enters the separator.
- This valve 28 comprises a pair of solenoids 100 and 102, operating a double poppet shut ofi valve 104 having a spring 106 urging it to closed position.
- Gas discharged by the poppet valve is led through duct 1% overboard or to a location outside of the tank.
- the vent from the inside to the outside of tank 32 in this modification consists of the duct 34 submerged in the tank 32, the orifice 90, the valve 26, orifice 94, rotor 22, duct 96, tubes of heat exchanger 24, duct 98, valve 28 and duct 108 discharging outside the tank.
- Pressure relief means for a storage tank for a pressurized mixture of gas and liquid comprising, a vent passage submerged in said tank and connecting the inside with the outside of said tank, a centrifuge in said tank, forming a part of said passage, receiving gas and liquid from said tank and separating said received gas and liquid and having a continuously open outlet in said tank returning liquid from said centrifuge to the mixturein the portion of the tank surrounding said centrifuge, and having a gas outlet in said passage, a motor actuated by the flow of gas discharged from said centrifuge through said gas outlet and passage for operating said centrifuge, means blocking said vent passage and means responsive to the pressure in said tank controlling said blocking means.
- Vent means as claimed in claim 2 including a second blocking means blocking the discharge from 'said motor and a second means for controlling said second blocking means.
- a centrifuge and a fluid motor drivingly connected with said centrifuge arranged in series in. a normally closed storage container pressure relief vent adapted to vent gas from a pressurized heterogeneous mixture of gas and liquid in said container when the pressure in said container exceeds a predetermined. amount
- said centrifuge having a mixture inlet in said container for receiving a stneam of said mixture from said container, at gas outlet in said vent, and a gas and liquid outlet in said container, means conducting gas separated from said mixture stream by said centrifuge and urged through said gas outlet and vent by the pressure difference between the inside and outside of said container to said motor to which said valve controls said conducting means.
- a combination as claimed in claim 5 including a shut-off valve down stream of the said combination.
- a storage device adapted to contain a volatile liquid in a zero gravity environment, a vent passage in the wall of the device having an inlet submerged in the inherent mixture of liquid and gas freely floating in said device and including pressure responsive means responsive to the pressure inside said device for releasing gases from said device upon the vapor pressure in the device reaching a predetermined value, means responsive to the flow of fluid in said vent passage for extracting power therefrom, fan means in the device operatively connected to said power extracting means for pumping the inherent mixture of liquid and gas freely floating in the device, said fan means including a centrifuge for agglomerating the liquid particles, and means for returning said liquid particles from said combined fan and centrifuge to a predetermined region within said device.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Centrifugal Separators (AREA)
Description
ELTAy oR E T AL I 3,107,988
I LIQYQUIYD VAPOR SEPARATOR I Filed Sept lzijleeo :1 4 Sheets-Sheet 1- A 4 A IN VEN TOPS HERBERT 5. TA FLOR EORGE GRANNENBERG MART/N RMAC/(LIN A r ToAwgr Oct. 22, 1963 Filed Sept. 12, 1960 H. E. TAYLOR ETAL LIQUID VAPOR SEPARATOR 4 Sheets-Sheet 2 INVENTOPS HERBERT E. TAYLOR GEORGE C. RA/VNENBERG MART/N R. MAC/(LIN ATTORMEV Oct. 22, 1963 AY ETAL 3,107,988
' LIQUID VAPOR SEPARATOR 4 Sheets-Sheet 55 Filed Sept. 12. 1960 s mmmm u M m NENM. T in A MR. 64 m 55m. Hm m m G Oct. 22, 1963 H. E. TAYLOR ETAL 3,107,988
LIQUID VAPOR SEPARATOR Filed Sept. 12, 1960 4 Sheets-Sheet 4 NVE N TOPS AT TOP/YE) 3,107,988 LIQUID VAPOR SEPARATOR Herbert E. Taylor, Longmeadow, and George C. Rannenberg, Agawarn, Mass, and Martin R. Macklin, Bloomfield, Conn, assignors to United Aircraft Corporation,
East Harfiord, Conn, a corporation of Delaware Filed Sept. 12, 1960, Ser. No. 55,339 8 Claims. (Cl. 55-311) -This invention relates to tank venting mechanism and particularly to mechanism utilizing energy in the vent stream for separating vapor from liquid in the stream, comprising a heterogeneous mixture of vapor and liquid such as would be present in a tank of cryogenic material, such as liquid hydrogen, in a zero gravity field.
In the interest of fuel or liquid conservation in a receptacle containing a volatile cryogenic material, such as liquid hydrogen, it is desirable to vent only the vapor or gas from the receptacle and retain the liquid. The receptacle may be subject to radiant heat from the sun or other heat source which will tend to heat the liquid and change some portions of the liquid to the vapor state with a consequent increase in the pressure in the receptacle. Because the vapor and liquid are intermingled and there is no well-defined separation under some conditions, such as a zero gravity field, a vent located anywhere in the tank would vent both vapor and liquid indiscriminately and mechanism supported anywhere in the tank would, under those conditions, be submerged in the mixture.
An object of this invention is to provide vent control mechanism which will select the vapor as the material to be vented from a pressurized container of a heterogeneous mixture of vapor and liquid, and retain the liquid.
Other objects and advantages will be apparent from the following specification and the accompanying drawings in which:
FIGURE 1 is a schematic showing of the vent and separator installed in a receptacle.
FIGURE 2 is a sectional view of the vent motor and separator.
FIGURE 3 is a plan view of the motor showing the pressure regulating valve and control.
FIGURE 4 is a sectional view on line 4-4 of FIG- URE 5 of a modified form of motor, separator, and relief valve, installed in a receptacle with the outlet valve removed.
FIGURE 5 is a front elevation showing the connections to the heat exchanger and the control valve.
FIGURE 6 is a sectional view of the control valve.
The device shown in FIGURES 1 to 3 essentially consi-sts of a centrifugal separator indicated generally at 10 powered by a positive displacement motor 12. and a pressure regulating and shut-off valve 14. This mechanism is all arranged in a tank vent 16. The vent separator is composed of an axial fiow fan 18 for establishing the centrifugal field in separating the liquid and gas. A diffuser 20 is provided for reducing the velocity of the fluid flow returning to the tank. The gas separated by the centrifugal field created by the fan 18 is used to power the positive displacement gear motor 12 and is then vented overboard through the pressure regulating valve 14. All leakage paths through the vent separator have been located upstream of the valve 14 so that the valve leakge will be the only leakage from the system.
The modification shown in FIGS. 4, 5, and 6 while broadly similar to the device shown in FIGS. 1-3 consists of a centrifugal separator indicated generally at 10, powered by a simple reaction turbine 22, a tube-type heat exchanger 24, a pressure regulating valve, and a solenoid operated shut-01f valve 28 all, a-s-shown in FIGS. 4, 5 and 6, supported in a receptacle from one of the walls 32 of the receptacle by suitable means, such as bolts 31, and under zero gravity conditions submerged in the mixture in the receptacle. The separator is composed of an axial flow fan for establishing the centrifugal field and in separating the liquid and gas. The gas to be vented is separated by the fan and passed through the direct acting, pressure regulator 26 located in the main housing 27 of the assembly before it enters the turbine 22. Because a temperature drop is experienced by the gas in passing through the turbine 22, and because some liquid droplets may be present, a heat exchanger 24 is incorporated to transfer heat from the mixture inside of the tank or receptacle to the cooled gas being vented. A shut-off valve 28 is provided down-stream of the heat exchanger 24 in the vented gas line. This valve 28 is solenoid-ac-tuated'and manually controlled to both the open and closed positions. A switch on the valve may be used to indicate the valve position.
Referring now to FIGURES l to 3, the tank or receptacle to be vented is indicated at 32, and the vent 16 connects the interior of the tank with the exterior thereof. The separator mechanism including the separator 10 and the motor 12 is located in the vent 16 and forms a part thereof. The vent and separator mechanism may be supported in the tank in any suitable manner such as on one of the tank walls or from any other suitable support. A duct 34 forming pant of the vent 16- is supported in the tank from the main body 36 of the separator and forms the outer casing for the fan 18 and may be partitioned from the remainder of the tank by a bafiie 37 if desired. Fan blades 38 are supported on a shaft 40 which is supported in bearings 42 and 44 and is directly connected with one of the gears 46 of the gear motor 12. The fan 18 is designed to impart a swirling motion to the fluid received in the duct 34 and assists the pressure difference between the inside and the outside of the tank in moving the fluid through the duct 34. The swirling motion will act as a centrifuge to drive the heavier or liquid particles toward the periphery of the duct, thus displacing the lighter or gaseous particles toward the fan shaft 40. Due to the pressure diiference between the inside and the outside of the tank, the gas particles will be forced through the orifice 48 into the hollow interior 50 of the shaft 40, and will be vented through the orifice 5-2 to the annulus 54 and then through duct 56 to the gear motor or expansion device 12. The expansion device will be driven by these pressurized gases and drive the shaft 40 and the fan 18. The liquid particles centrifuged to the outside of the duct 34 together with excess gas which did not pass through orifice 48 will pass through the diffuser 2@ to efliciently change their velocity into static pressure and will then be discharged directly back into the portion of the tank surrounding the separator. If the flow en tering the duct 34 is large enough to contain sur'licient gas, it will be possible to separate this gas from the mixture of liquid and gas to drive the expansion device 12 without the loss of any or any appreciable amount of liquid. Any excess of gas, beyond that required to drive the motor 12, will of course be returned to the portion of the tank surrounding the separator along with the separated liquid.
The gas discharged from the motor 12 is led through the portions 60 of the vent 16 to the pnessure regulating and shut-off valve 14. The valve 14 comprises a springpressed valve member 62 blocking the passage 60 from the outlet passage '64 of the vent 16 leading overboard or to ambient. Plunger 62 in addition to being urged to closed position by spring 66 is also urged to closed position by fluid pressure acting on the surface 68 of the plunger 62. Fluid is led through line 71, from the passage 56 leading to the gear motor, into the chamber 70 to act on the surface 68. A restriction 72 limits the rate of flow of fluid to the chamber 70. Fluid may be vented to ambient, by connections not shown, from the chamber 70, faster than it is admitted past restriction 72, by the valve 74 controlled by pressure in the bellows 76 which is connected by conduit 78 with the tank 32. Bellows 8d, the outside of which is connected, by connections not shown, with ambient, is balanced between springs 82 and 84 and as this device is intended to operate in the outer atmosphere where the pressure is substantially zero the pressure outside of the bellows is substantially zero. A valve 86 controlled by solenoid 88 is used to block the exit passage from the valve 74 and thus hold the valve 62 in closed position, when desired.
The modification as shown in FIGURES 4 to 6 is broadly similar to that shown in FIGS. 1-3 and differs from that previously described mainly in the location of the pressure regulating valve between the separator and the turbine and the incorp-oraiton of a heat exchanger in the turbine exhaust. Also FIGURES 2 and 4 differ in the type of expansion device shown. FIGURE 2 shows positive displacement; FIGURE 4, a turbine. The actual configuration of expansion device used in any particular application is dependent on considerations such as cost and efficiency. The fan 30' having blades 38 supported on a shaft 40 is located similar to that shown in FIGS. 1-3 in a duct 34, a portion of which acts as a casing for the fan. The shaft 40 is supported in bearings 42. and 44 and has the turbine wheel 22secured to the upper end thereof. The fan 30 imparts a swirling motion to the mixture of gas and liquid received in the duct 34 and acts as a centrifuge toforce the liquid towards the outer periphery of the duct 34- and discharge it through the diffuser 20. A heat exchanger 24 is arranged around the outer periphery of the diffuser 2d and the liquid and excess gas discharged by the fan 30 passes through this heat exchanger, around the exterior of the heat exchanger tubes, on its Way back to the portion of the tank surrounding the separator Gas to be vented is separated from the mixture of gas and liquid by the centrifuge action of the fan and passes through the orifice 90 around the outside of shaft 40 and under the spring-pressed poppet valve 26, supported on evacuated bellows 92. After opening and passing the poppet valve 26, the gas passes through orifice 94 through the interior of the turbine rotor 22 to be discharged at its periphery. The discharged gas which is cooled due to expansion through the turbine and because of the work done in turning the fan is led through duct 96 to a chamber 97, partitioned off by a partition 99, in a manifold 131 and thence to the interior of the tubes of the heat exchanger 24. After passing through the heat exchanger and cooling the liquid and gas being returned from the separator to the portion of the tank surrounding the separator, the discharged gas is led through a chamber 108 formed in the manifold 101 by the partition 99 and then through duct 98 to the shut-off valve 28. Alternatively the heat exchanger may be located in duct 35 to cool the mixture before it enters the separator. This valve 28 comprises a pair of solenoids 100 and 102, operating a double poppet shut ofi valve 104 having a spring 106 urging it to closed position. Gas discharged by the poppet valve is led through duct 1% overboard or to a location outside of the tank. The vent from the inside to the outside of tank 32 in this modification consists of the duct 34 submerged in the tank 32, the orifice 90, the valve 26, orifice 94, rotor 22, duct 96, tubes of heat exchanger 24, duct 98, valve 28 and duct 108 discharging outside the tank.
While the above described mechanism is intended as the normal means for relieving excess pressure in the tank, it Will be appreciated that additional or safety relief valve mechanism may be provided to provide a vent in the event of failure of the normal venting mechanism.
It is to be understood that the invention is not limited to the specific embodiments herein illustrated and described, but may be used in other ways without departure from its spirit, and that various changes can be" made which would come within the scope of the inventionwhich is limited only by the appended claims.
We claim:
1. Pressure relief means for a storage tank for a pressurized mixture of gas and liquid comprising, a vent passage submerged in said tank and connecting the inside with the outside of said tank, a centrifuge in said tank, forming a part of said passage, receiving gas and liquid from said tank and separating said received gas and liquid and having a continuously open outlet in said tank returning liquid from said centrifuge to the mixturein the portion of the tank surrounding said centrifuge, and having a gas outlet in said passage, a motor actuated by the flow of gas discharged from said centrifuge through said gas outlet and passage for operating said centrifuge, means blocking said vent passage and means responsive to the pressure in said tank controlling said blocking means.
2. Vent means as claimed in claim 1 in which the blocking means is located between the centrifuge and the motor. i
3. Vent means as claimed in claim 2 including a second blocking means blocking the discharge from 'said motor and a second means for controlling said second blocking means.
4. Vent means as claimed in claim 1 in which the blocking means is located at the discharge of said motor.
5. In combination, a centrifuge and a fluid motor drivingly connected with said centrifuge arranged in series in. a normally closed storage container pressure relief vent adapted to vent gas from a pressurized heterogeneous mixture of gas and liquid in said container when the pressure in said container exceeds a predetermined. amount, said centrifuge having a mixture inlet in said container for receiving a stneam of said mixture from said container, at gas outlet in said vent, and a gas and liquid outlet in said container, means conducting gas separated from said mixture stream by said centrifuge and urged through said gas outlet and vent by the pressure difference between the inside and outside of said container to said motor to which said valve controls said conducting means.
7. A combination as claimed in claim 5 including a shut-off valve down stream of the said combination.
8. A storage device adapted to contain a volatile liquid in a zero gravity environment, a vent passage in the wall of the device having an inlet submerged in the inherent mixture of liquid and gas freely floating in said device and including pressure responsive means responsive to the pressure inside said device for releasing gases from said device upon the vapor pressure in the device reaching a predetermined value, means responsive to the flow of fluid in said vent passage for extracting power therefrom, fan means in the device operatively connected to said power extracting means for pumping the inherent mixture of liquid and gas freely floating in the device, said fan means including a centrifuge for agglomerating the liquid particles, and means for returning said liquid particles from said combined fan and centrifuge to a predetermined region within said device.
References Cited in the file of this patent UNITED STATES PATENTS Kirsch Sept. 8, 1931 Dodge Oct. 8, 1940 Anderson Aug. 14, 1956 Dueker Dec. 16, 1958 Anderson Jan. 13, 1959 Hunter Aug. 4, 1959 Reistle Oct. 4, 1960 Woodmansee Nov. 1, 1960 FOREIGN PATENTS Great Britain AD. 1875
Claims (1)
1. PRESSURE RELIEF MEANS FOR A STORAGE TANK FOR A PRESSURIZED MIXTURE OF GAS AND LIQUID COMPRISING, A VENT PASSAGE SUBMERGED IN SAID TANK AND CONNECTING THE INSIDE WITH THE OUTSIDE OF SAID TANK, A CENTRIFUGE IN SAID TANK, FORMING A PART OF SAID PASSAGE, RECEIVING GAS AND LIQUID FROM SAID TANK AND SEPARATING SAID RECEIVED GAS AND LIQUID AND HAVING A CONTINUOUSLY OPEN OUTLET IN SAID TANK RETURNING LIQUID FROM SAID CENTRIFUGE TO THE MIXTURE IN THE PORTION OF THE TANK SURROUNDING SAID CENTRIFUGE, AND HAVING A GAS OUTLET IN SAID PASSAGE, A MOTOR ACTUATED BY THE FLOW OF GAS DISCHARGED FROM SAID CENTRIFUGE THROUGH SAID GAS OUTLET AND PASSAGE FOR OPERATING SAID CENTRIFUGE, MEANS BLOCKING SAID VENT PASSAGE AND MEANS RESPONSIVE TO THE PRESSURE IN SAID TANK CONTROLLING SAID BLOCKING MEANS.
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US55339A US3107988A (en) | 1960-09-12 | 1960-09-12 | Liquid vapor separator |
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US55339A US3107988A (en) | 1960-09-12 | 1960-09-12 | Liquid vapor separator |
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US3107988A true US3107988A (en) | 1963-10-22 |
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US55339A Expired - Lifetime US3107988A (en) | 1960-09-12 | 1960-09-12 | Liquid vapor separator |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3209518A (en) * | 1961-04-19 | 1965-10-05 | Midland Ross Corp | Device and method for separating a liquid from a gas |
US3257780A (en) * | 1963-10-18 | 1966-06-28 | James E Webb | Zero gravity separator |
US3397512A (en) * | 1966-12-28 | 1968-08-20 | James E. Webb | Vapor-liquid separator |
US4323369A (en) * | 1979-05-07 | 1982-04-06 | Donaldson Company, Inc. | Air cleaner and ventilator |
US4832709A (en) * | 1983-04-15 | 1989-05-23 | Allied Signal, Inc. | Rotary separator with a bladeless intermediate portion |
US4840645A (en) * | 1983-04-15 | 1989-06-20 | Allied-Signal Inc. | Rotary separator with a porous shroud |
US20100300051A1 (en) * | 2007-08-29 | 2010-12-02 | Kristof Adrien Laura Martens | Liquid separator |
WO2015018816A1 (en) * | 2013-08-08 | 2015-02-12 | Sanofi-Aventis Deutschland Gmbh | Recovery assembly for cryopreservation applications |
EP3537026A1 (en) * | 2018-03-06 | 2019-09-11 | L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude | System, device and method for controlling the pressure of a fluid tank |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1822659A (en) * | 1928-07-05 | 1931-09-08 | Kirsch Michael | Means for extracting air from water |
US2216939A (en) * | 1939-02-18 | 1940-10-08 | Eugene W Dodge | Rotary gas and oil separator |
US2758672A (en) * | 1953-09-29 | 1956-08-14 | Curtiss Wright Corp | Engine crankcase breather and air-oil separator |
US2864461A (en) * | 1955-03-23 | 1958-12-16 | Wagner Electric Corp | Integrated oil separating system for gas compressors |
US2868324A (en) * | 1955-12-05 | 1959-01-13 | Robert J Anderson | Vent line centrifuge |
US2897917A (en) * | 1957-11-15 | 1959-08-04 | Fairchild Engine & Airplane | Apparatus for separating moisture and condensable vapors from a gas |
US2954841A (en) * | 1956-11-16 | 1960-10-04 | Jersey Prod Res Co | Centrifugal separator |
US2958394A (en) * | 1957-09-23 | 1960-11-01 | John B Woodmansee | Automatic moisture extractor for compressed air lines |
-
1960
- 1960-09-12 US US55339A patent/US3107988A/en not_active Expired - Lifetime
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
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US1822659A (en) * | 1928-07-05 | 1931-09-08 | Kirsch Michael | Means for extracting air from water |
US2216939A (en) * | 1939-02-18 | 1940-10-08 | Eugene W Dodge | Rotary gas and oil separator |
US2758672A (en) * | 1953-09-29 | 1956-08-14 | Curtiss Wright Corp | Engine crankcase breather and air-oil separator |
US2864461A (en) * | 1955-03-23 | 1958-12-16 | Wagner Electric Corp | Integrated oil separating system for gas compressors |
US2868324A (en) * | 1955-12-05 | 1959-01-13 | Robert J Anderson | Vent line centrifuge |
US2954841A (en) * | 1956-11-16 | 1960-10-04 | Jersey Prod Res Co | Centrifugal separator |
US2958394A (en) * | 1957-09-23 | 1960-11-01 | John B Woodmansee | Automatic moisture extractor for compressed air lines |
US2897917A (en) * | 1957-11-15 | 1959-08-04 | Fairchild Engine & Airplane | Apparatus for separating moisture and condensable vapors from a gas |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3209518A (en) * | 1961-04-19 | 1965-10-05 | Midland Ross Corp | Device and method for separating a liquid from a gas |
US3257780A (en) * | 1963-10-18 | 1966-06-28 | James E Webb | Zero gravity separator |
US3397512A (en) * | 1966-12-28 | 1968-08-20 | James E. Webb | Vapor-liquid separator |
US4323369A (en) * | 1979-05-07 | 1982-04-06 | Donaldson Company, Inc. | Air cleaner and ventilator |
US4832709A (en) * | 1983-04-15 | 1989-05-23 | Allied Signal, Inc. | Rotary separator with a bladeless intermediate portion |
US4840645A (en) * | 1983-04-15 | 1989-06-20 | Allied-Signal Inc. | Rotary separator with a porous shroud |
US20100300051A1 (en) * | 2007-08-29 | 2010-12-02 | Kristof Adrien Laura Martens | Liquid separator |
US8372173B2 (en) * | 2007-08-29 | 2013-02-12 | Atlas Copco Airpower, Naamloze Vennootschap | Liquid separator |
WO2015018816A1 (en) * | 2013-08-08 | 2015-02-12 | Sanofi-Aventis Deutschland Gmbh | Recovery assembly for cryopreservation applications |
EP3537026A1 (en) * | 2018-03-06 | 2019-09-11 | L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude | System, device and method for controlling the pressure of a fluid tank |
FR3078765A1 (en) * | 2018-03-06 | 2019-09-13 | L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Procedes Georges Claude | SYSTEM, DEVICE AND METHOD FOR REGULATING THE PRESSURE OF A FLUID RESERVOIR |
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