Movatterモバイル変換


[0]ホーム

URL:


US3130561A - Insulation device - Google Patents

Insulation device
Download PDF

Info

Publication number
US3130561A
US3130561AUS149239AUS14923961AUS3130561AUS 3130561 AUS3130561 AUS 3130561AUS 149239 AUS149239 AUS 149239AUS 14923961 AUS14923961 AUS 14923961AUS 3130561 AUS3130561 AUS 3130561A
Authority
US
United States
Prior art keywords
vacuum
pressure
space
torr
pump
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US149239A
Inventor
Jr Milo P Hnilicka
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
National Research Corp
Original Assignee
National Research Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from CH769361Aexternal-prioritypatent/CH395669A/en
Application filed by National Research CorpfiledCriticalNational Research Corp
Priority to US149239ApriorityCriticalpatent/US3130561A/en
Application grantedgrantedCritical
Publication of US3130561ApublicationCriticalpatent/US3130561A/en
Anticipated expirationlegal-statusCritical
Expired - Lifetimelegal-statusCriticalCurrent

Links

Images

Classifications

Definitions

Landscapes

Description

April 28, 1964 M. P. HNlLlcKA, JR .Y 3,130,551
INSULATION DEVICE Filed Nov. l, 1961 PRESSURE RESPONSIVE United States Patent O 3,130,561 INSULATIQN DEVICE Milo P. Hnilicka, Jr., Concord, Mass., assigner to National Research Corporation, Cambridge, Mass., a corporation of Massachusetts Filed Nov. 1, 1961, Ser. No. 149,239 4 Claims. (Cl. 62-331) This invention relates to the insulation of containers and particularly to maintaining the eiciency of vacuum insulation of containers for cryogenic liquids and other materials conventionally stored or transported at very low temperatures.
Recently developed superinsulations of the general type described in British Patent 853,585 or my copending application S.N. 842,139, liled September 24, 1959, now Patent No. 3,018,016, derive their impedance to heat ilux from the elect of multiple radiation barriers. The absence of residual gas conduction by evacuation to high vacuum is essential to proper function of all these superinsulations.
Thus, a major problem involved in the use of these types of insulation is that of maintaining a high vacuum during the required insulation period. For example, should a slight leak occur the absolute pressure of the system will rise md the thermal conductivity of the system will increase. This increase is due to the increase in thermal conduction by the increased residual gas in the insulated vacuum space.
Accordingly, it is a principal object of the invention to provide an insulation unit of simple construction which will maintain a high insulation vacum over long insulation periods.
Another object of the present invention is to provide an insulated container and means by which the vacuum is selfrenewing and self-sustaining.
A further object of this invention is to provide an insulation container which Will sustain a high vacuum in the evacuated space and which is a complete unit having virtually no moving parts.
Other objects of the invention will in part be obvious and will in part appear hereinafter.
The invention accordingly comprises the apparatus possessing the construction, combination of elements and arrangement of parts which are exemplilied in the following detailed disclosure and the scope of the application of which will be dened in the claims.
For a fuller understanding of the nature and objects of the invention, reference should be had to the following detailed description taken in connection with the accompanying drawing which is a schematic, diagrammatic sectional illustration of one preferred form of apparatus embodying the present invention.
Briey stated, the objects of the invention are accomplished by providing a vacuum-tight container for an adsorbent material which is preferably positioned within the insulated container so as to be cooled to cryogenic temperatures. The adsorbent material is connected by suitable conduit means to the discharge port of a diffusion pump. The diffusion pump is positioned outside of the vacuum vessel but connected so that it can evacuate the insulating portion of thevessel. Thus there is provided a novel arrangement wherein the adsorbent material, when at cryogenic temperature, acts in the capacity of a backing pump for the diffusion pump. The advantages of such an arrangement will now be described in detail.
It has been proposed in prior art methods that an adsorbent material be inserted into the evacuated insulation space to maintain the Vacuum. According to prior art methods, the adsorbent material is arranged in the vacuum space so that it is in direct communication with the Vacuum space.
In order to chill the adsorbent it has been the practice to place the adsorbent in Contact with the insulated vessel so that when the vessel is lled with a liqueed gas, for example, the adsorbent will come to the same low temperature as the liqueed gas. An adsorbent such as calcium zeolite A described in U.S. Patent No. 2,900,800, when at -l C. and at l torr (1 mm. Hg abs.) can adsorb 200 volumes of gas at standard temperature and pressure (STP) for each volume of adsorbent. At the same temperature -180 C.) but at a pressure of 10*5 torr, the same adsorbent can adsorb only 0.07 volume of gas at STP for each Volume of adsorbent.
According to prior art methods, one liter of zeolite A, for example, when placed in the evacuated space at a pressure of 10`5 torr and at a temperature of -180 C., can keep adsorbing gas at 10 liters per second for 170 hours.
In contrast, one liter of zeolite A, according to the present invention, can be placed in a vacuum-tight container comprising an adsorbent space which is preferably positioned in heat transfer relation to the liqueed gas so as to be chilled to the temperature of the liqueed gas (eg. 180 C.). The adsorbent space is not directly connected open to the evacuated insulation space (which is at 10-5 torr) but is, instead, connected to the outlet of a pump which is arranged to pump the insulation space. This pump, which can be a diffusion pump, has inherently a high compression ratio, allowing discharge into a forepressure of for example 1 torr. Hence, the diusion pump pumps gas from the evacuated insulation space to maintain a pressure of 10*5 torr in the insulation space and discharges the pumped gas, after compression, into the adsorbent space at a pressure which can attain 1 torr. Thus the zeolite A adsorbent, while at a temperature of 180 C., will be adsorbing gas at l torr and not at 10-5 torr as in prior art methods and apparatus. Since the adsorption capacity rapidly increases with pressure, 1 liter of zeolite A can hold 200 liters of gas at l torr, and the liter of zeolite A will keep adsorbing gas at 10 liters/sec. for 432,000 hours or about 2500 times longer than that of the prior art apparatus.
The advantages of the present invention are more readily apparent when the insulation period is determined for a system having a leak, for example, of 0.1 micron liters per second (1 l0*4 torr liters/ second). One volume of zeolite A adsorbent at -180 C. and at a pressure of 10-5 torr could maintain the evacuated space at 10-5 torr for approximately six days. The same adsorbent material at -180 C., when arranged to adsorb pumped gas, after compression by a diusion or other suitable pump to a pressure level of 1 torr, can maintain the evacuated space at 105 torr in the presence of a leak of 0.1 micron liter per second for approximately 48 years.
Referring now to the drawing there is shown one preferred embodiment of the present invention. The insulated container comprises aninner vessel 10 adapted to conne a cryogenic liquid 12, the liquid being at a temperature of less than K. and at about atmospheric pressure. Anouter chamber 13 surrounds theinner chamber 10 and defines therewith a space 14 which is evacuated to a free air pressure on the order of 10*2 to l08 microns Hg abs. (10-5 to l0*10 torr). Space 14 contains a superinsulation schematically indicated at 15. Adiffusion pump 15 is connected by aconduit 18 to the space 14 to be evacuated `so as to maintain the evacuated space 14 under high vacuum.
An adsorbent material 20 is held in heat transfer relationship with the cryogenic liquid by means of awall 22 separating an end portion of thetank 10 to provide aseparate chamber 24.Chamber 24 is connected by means of apipe 26 to the foreline ofdiffusion pump 16 and also to the backing pump 23. Three valves, (30, 32 and 34) are provided to permit operation of the backing pump and diffusion pump in any predetermined sequence.` Avalve 36 is also provided for isolating the diffusion pump from the insulation space 14. A suitable pressure responsive element 3S is preferably provided for monitoring the vacuum in the insulation space 14. In a preferred embodiment of the invention the pressure responsive element automatically controls the operation of the diffusion pump and turns it on when the pressure in space 14 has risen much above 1 X 10-5 torr- In a preferred embodiment of the invention the inner tank is formed of stainless steel and theinsulation 15 comprises crinkled metallized plastic of the type described in my copending application, Serial No. 842,- 139, filed September 24, 1959. The adsorbent material is preferably a commercially available zeolite of the type described in U. S. Patent 2,900,800. Thediffusion pump 16 is a standard oil vapor or mercury vapor diffusion pump and the pump 2S can be a small mechanical vacuum pump. When the insulated container is mounted on a trailer, for example, the backing pump 2S can be removed from the system after the initial evacuation thereof and the adsorbent 20 then acts as the backing pump for thediffusion pump 16.
In the operation of the system shown with no cryogenic liquid in thetank 10, theadsorbent chamber 24 is rst preferably evacuated while the adsorbent 25d is at arnbient temperature. This is achieved by operating the backing pump 2S withvalves 34 and 32 open and valve closed. When a predetermined low pressure of the order of l torr is obtained, thevalve 32 is closed andvalves 30 and 36 are opened to evacuate the insulation space 14. With the diffusion pump operating, this space is evacuated to a low pressure less than 104 torr, Thereaftervalve 32 is opened whilevalves 36, 30 and 34 are closed and thetank 10 is lled with cryogenic liquid 12. This will tend to lower the pressure in the insulation space 14 even below the pressure obtained with the diffusion pump. Assuming that there are no leaks in the system it will remain indenitely at this low pressure. However, if there is a small leak, the pressure in the insulation space 14 will gradually rise. When it reaches a pressure on the order of l l0r5 torr, the pressure sensing element 3S starts thediffusion pump 16, opens thevalve 36 as well asvalve 30. As a result of this, gases leaking into the space 14 are pumped out through thediffusion pump 16 where they are compressed up to a pressure on the order of 1 torr and adsorbed by the cold adsorbent 20. When the pressure in the insulation space 14 drops to a predetermined low value thepump 16 is turned oif and the Valves 36 and 30 are again closed. During this operation it is apparent that backing pump 2g serves no useful purpose and need not be connected to the system and can be disconnected after initial pumpdown.
While one preferred embodiment of the invention has been described above, numerous modifications can be made without departing from the spirit of the invention. For example, numerous other adsorbents such as carbon, silica gel, alumina and other adsorbent materials having high adsorptive capacity at low temperature can be employed. Additionally a heater can be provided for assisting in initial pumpdown of the adsorbent. While a diffusion pump is preferred to compress the gases from the insulation space, other types of pumps may be employed. Sinu'larly, other types of multiple radiation shields may be utilized in place of the preferred metallized plastic type described in my above-mentioned copending application.
Depending upon the use to which the insulated container is to be subjected, it may be made more or less automatic in its operation. Thus, for example, the pressureresponsive element 38 can be utilized to start an automatic sequence of operations which will involve the heating of the diffusion pump and opening ofvalves 36 and 30 to permit evacuation of the space 14. When a predetermined low pressure has been achieved, the reverse sequence of operations can be automatically achieved by the pressure responsive element to provide closing of thevalves 30 and 36 and removal of power from the diifusion pump. When such a system is mounted on a trailer, it can be battery-operated to provide complete independence of any external power supply. While it is preferred that space 14 be initially evacuated, it can have a pressure of a condensible gas such as CO2 which is completely condensed to evacuate the space when a cryogenic liquid is provided in theinner tank 10.
Since certain changes may be made in the above apparatus without departing from the scope of the invention herein involved, it is intended that all matter contained in the above description shall be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. An insulated vessel comprising an inner chamber to be maintained at a predetermined low temperature below about K., an outer chamber spaced from said inner chamber and sealed to form a vacuum-tight insulation space therebetween, and means for maintaining said vacuum-tight insulation space at a pressure less than 10-5 torr, said means comprising a vacuum-tight container having therein an adsorbent material arranged in heat exchange contact with said inner chamber so as to be cooled to a temperature below 100 K. and pump means for removing gases from said vacuum-tight insulation space and compressing said gases to a pressure on theorder of 1 torr, the discharge from said pump being connected to the container for said adsorbent material so that said adsorbent material can adsorb said compressed gases.
2. An insulated vessel comprising an inner chamber to be maintained at a predetermined low temperature below about 100 K., an outer chamber spaced from said inner chamber and sealed to form a Vacuum-tight insulation space therebetween, and means for maintaining said vacuum-tight insulation space at a pressure less than 1 105 torr, said means comprising a vacuumtight container having therein an adsorbent material arranged in heat exchange contact with said inner chamber so as to be cooled to a temperature below 100 K., pump means for removing gases from said vacuum-tight insulation space and compressing said gases to a pressure which is at least 100 times greater than the pressure to be maintained in said insulation space, and means for conducting said compressed gases to said cold adsorbent material.
3. An insulated Vessel comprising an inner chamber to be maintained at a predetermined low temperature, said inner chamber being defined by a rst wall, a second wall outside of said rst wall and spaced therefrom, said walls being sealed to form a vacuum-tight space therebetween, a vacuum-tight container of gas-adsorbent material constructed and arranged to be in thermal contact with said inner chamber, a plurality of radiant heat barriers surrounding said inner wall and said vacuum-tight con-V tainer, conduit means in said second wall connecting said vacuum-tight space with a diffusion pump and conduit means constructed and arranged so that said adsorbent material receives gases discharged frorn said diffusion pump.
4. An insulated vessel comprising an inner chamber to be maintained at a predetermined low temperature below about 100 K., an outer chamber spaced from said inner chamber and sealed to form a vacuum-tight insulation space therebetween, a plurality of radiant heat shields in said insulation space, means for maintaining said vacuum-tight insulation space at a pressure less than 1x10-5 torr, said means comprising a vacuumtight container having therein an adsorbent material arranged in heat exchange contact with said inner chamber so as to be cooled to a temperature below 1007 K., a vacuum pump capable of pumping said insulation space to a pressure less than 1 105 torr and compressing said gases to a pressure which is at least 100 times greater than the pressure to be maintained in said insulation space, and means for conducting said compressed gases to said adsorbent material, and means responsive to the pressure in said insulation space for controlling the operation of said vacuum pump.
References Cited in the file of this patent UNITED STATES PATENTS Jackson et lal Sept. 21, 1943 Hippie Mar. 22, 1949 Loveday May 11, 1954 Matsch Nov. 7, 1961

Claims (1)

  1. 2. AN INSULATED VESSEL COMPRISING AN INNER CHAMBER TO BE MAINTAINED AT A PREDETERMINED LOW TEMPERATURE BELOW ABOUT 100*K., AN OUTER CHAMBER SPACED FROM SAID INNER CHAMBER AND SELAED TO FORM A VACUUM-TIGHT INSULATION SPACE THEREBETWEEN, AND MEANS FOR MAINTAINING SAID VACUUM-TIGHT INSULATION SPACE AT A PRESSURE LESS THAN 1X10**-5 TORR, SAID MEANS COMPRISING A VACUUMTIGHT CONTAINER HAVING THEREIN AN ADSORBENT MATERIAL ARRANGED IN HEAT EXCHANGE CONTACT WITH SAID INNER CHAMBER SO AS TO BE CODED TO A TEMPERATURE BELOW 400*K., PUMP MEANS FOR REMOVING GASES FROM SAID VACUUM-TIGHT INSULATION SPACE AND COMPRESSING SAID GASSES TO A PRESSURE
US149239A1961-06-301961-11-01Insulation deviceExpired - LifetimeUS3130561A (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
US149239AUS3130561A (en)1961-06-301961-11-01Insulation device

Applications Claiming Priority (2)

Application NumberPriority DateFiling DateTitle
CH769361ACH395669A (en)1961-06-301961-06-30 Thermal insulation
US149239AUS3130561A (en)1961-06-301961-11-01Insulation device

Publications (1)

Publication NumberPublication Date
US3130561Atrue US3130561A (en)1964-04-28

Family

ID=25701940

Family Applications (1)

Application NumberTitlePriority DateFiling Date
US149239AExpired - LifetimeUS3130561A (en)1961-06-301961-11-01Insulation device

Country Status (1)

CountryLink
US (1)US3130561A (en)

Cited By (30)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3230727A (en)*1964-01-271966-01-25Union Carbide CorpVacuum insulated storage containers having improved vacuum maintenance means
US3230726A (en)*1964-01-271966-01-25Union Carbide CorpElastomeric connecting means for double-walled containers
US3425233A (en)*1966-08-261969-02-04United Aircraft CorpProcess and means for regulating the pressure and flow of a stored fluid
US3525452A (en)*1967-03-311970-08-25Linde AgMethod and device for thermally insulating a vessel
US3693367A (en)*1970-04-241972-09-26Leonard J Di PeriThermodynamic control device
US3724228A (en)*1970-07-301973-04-03Bendix CorpComposite insulation for cryogenic vessel
US3938347A (en)*1974-04-121976-02-17Optical Coating Laboratory, Inc.Level control apparatus and method for cryogenic liquids
US3942331A (en)*1974-07-081976-03-09The Dow Chemical CompanyCryogenic tank
US4011963A (en)*1973-06-151977-03-15The Dow Chemical CompanyCryogenic vessel
US4027379A (en)*1973-06-151977-06-07The Dow Chemical CompanyMethod of insulating cryogenic vessels
US4300356A (en)*1979-11-211981-11-17Union Carbide CorporationRefrigeration storage assembly
US4606196A (en)*1984-12-191986-08-19Union Carbide CorporationVacuum insulation system
US4667390A (en)*1984-12-191987-05-26Union Carbide CorporationVacuum insulation system method of manufacture
US5386706A (en)*1993-06-101995-02-07Praxair Technology, Inc.Low heat-leak, coherent-aerogel, cryogenic system
US5408832A (en)*1992-06-081995-04-25Saes Getters, S.P.A.Thermally insulating jacket and related process
US5412954A (en)*1992-09-161995-05-09L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Precedes Georges ClaudeApparatus for cryogenic treatment, such as air distillation
US5419139A (en)*1993-12-131995-05-30Martin Marietta CorporationComposite cryogenic tank apparatus
US5518138A (en)*1993-02-241996-05-21Saes Getters S.P.A.Unsulating jacket
US5542255A (en)*1994-05-041996-08-06Minnesota Valley Engineering, Inc.High temperature resistant thermal insulation for cryogenic tanks
US5625742A (en)*1993-07-081997-04-29Saes Getters S.P.A.Thermally insulating jacket under reversible vacuum utilizing hydrogen getter in combination with non-evaporable promoter getter
US5765379A (en)*1994-01-191998-06-16Elcold-Tectrade I/SThermal insulation system of the vacuum type
WO1999011990A1 (en)*1997-08-281999-03-11Messer Griesheim GmbhLow-temperature air separation installation
US6038867A (en)*1998-07-312000-03-21General Electric CompanyWide multilayer insulating blankets for zero boiloff superconducting magnet
US6155058A (en)*1997-04-102000-12-05Showa Denko K.K.Containerized refrigerant comprising refrigerant in disposable container
EP1353135A1 (en)*2002-04-082003-10-15Whirlpool CorporationVacuum insulated refrigerator cabinet and method for evacuating the gas-tight insulated wall thereof
WO2004029503A3 (en)*2002-09-272004-07-15Univ CaliforniaLightweight cryogenic-compatible pressure vessels for vehicular fuel storage
US20040250551A1 (en)*2001-08-222004-12-16Bayerische Motoren Werke AktiengesellschaftCryogenic tank for storing cryogenic fuel in a motor vehicle and method for using same
US20090283176A1 (en)*2008-05-162009-11-19Berry Gene DCryogenic Capable High Pressure Containers for Compact Storage of Hydrogen Onboard Vehicles
US20150300571A1 (en)*2014-04-162015-10-22Bayerische Motoren Werke AktiengesellschaftMethod for Producing a Tank, In Particular a Motor Vehicle Tank
US10794536B2 (en)2017-11-302020-10-06Cryogenic Fuels Inc.Vacuum acquisition systems and methods

Citations (4)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2329765A (en)*1941-11-121943-09-21James O JacksonLow temperature storage tank
US2465229A (en)*1944-09-071949-03-22Westinghouse Electric CorpVacuum trap
US2677938A (en)*1950-11-161954-05-11Union Carbide & Carbon CorpVacuum-insulated container and process for evacuating same
US3007596A (en)*1956-07-161961-11-07Union Carbide CorpThermal insulation

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2329765A (en)*1941-11-121943-09-21James O JacksonLow temperature storage tank
US2465229A (en)*1944-09-071949-03-22Westinghouse Electric CorpVacuum trap
US2677938A (en)*1950-11-161954-05-11Union Carbide & Carbon CorpVacuum-insulated container and process for evacuating same
US3007596A (en)*1956-07-161961-11-07Union Carbide CorpThermal insulation

Cited By (39)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3230727A (en)*1964-01-271966-01-25Union Carbide CorpVacuum insulated storage containers having improved vacuum maintenance means
US3230726A (en)*1964-01-271966-01-25Union Carbide CorpElastomeric connecting means for double-walled containers
US3425233A (en)*1966-08-261969-02-04United Aircraft CorpProcess and means for regulating the pressure and flow of a stored fluid
US3525452A (en)*1967-03-311970-08-25Linde AgMethod and device for thermally insulating a vessel
US3693367A (en)*1970-04-241972-09-26Leonard J Di PeriThermodynamic control device
US3724228A (en)*1970-07-301973-04-03Bendix CorpComposite insulation for cryogenic vessel
US4011963A (en)*1973-06-151977-03-15The Dow Chemical CompanyCryogenic vessel
US4027379A (en)*1973-06-151977-06-07The Dow Chemical CompanyMethod of insulating cryogenic vessels
US3938347A (en)*1974-04-121976-02-17Optical Coating Laboratory, Inc.Level control apparatus and method for cryogenic liquids
US3942331A (en)*1974-07-081976-03-09The Dow Chemical CompanyCryogenic tank
US4300356A (en)*1979-11-211981-11-17Union Carbide CorporationRefrigeration storage assembly
US4606196A (en)*1984-12-191986-08-19Union Carbide CorporationVacuum insulation system
US4667390A (en)*1984-12-191987-05-26Union Carbide CorporationVacuum insulation system method of manufacture
US5408832A (en)*1992-06-081995-04-25Saes Getters, S.P.A.Thermally insulating jacket and related process
USRE42467E1 (en)1992-06-082011-06-21Saes Getters S.P.A.Thermally insulating jacket and related process
US5412954A (en)*1992-09-161995-05-09L'air Liquide, Societe Anonyme Pour L'etude Et L'exploitation Des Precedes Georges ClaudeApparatus for cryogenic treatment, such as air distillation
US5518138A (en)*1993-02-241996-05-21Saes Getters S.P.A.Unsulating jacket
US5386706A (en)*1993-06-101995-02-07Praxair Technology, Inc.Low heat-leak, coherent-aerogel, cryogenic system
US5625742A (en)*1993-07-081997-04-29Saes Getters S.P.A.Thermally insulating jacket under reversible vacuum utilizing hydrogen getter in combination with non-evaporable promoter getter
US5419139A (en)*1993-12-131995-05-30Martin Marietta CorporationComposite cryogenic tank apparatus
US5765379A (en)*1994-01-191998-06-16Elcold-Tectrade I/SThermal insulation system of the vacuum type
US5542255A (en)*1994-05-041996-08-06Minnesota Valley Engineering, Inc.High temperature resistant thermal insulation for cryogenic tanks
US6155058A (en)*1997-04-102000-12-05Showa Denko K.K.Containerized refrigerant comprising refrigerant in disposable container
WO1999011990A1 (en)*1997-08-281999-03-11Messer Griesheim GmbhLow-temperature air separation installation
US6038867A (en)*1998-07-312000-03-21General Electric CompanyWide multilayer insulating blankets for zero boiloff superconducting magnet
US7036323B2 (en)*2001-08-222006-05-02Bayerische Motoren Werke AktiengesellschaftCryogenic tank for storing cryogenic fuel in a motor vehicle and method for using same
US20040250551A1 (en)*2001-08-222004-12-16Bayerische Motoren Werke AktiengesellschaftCryogenic tank for storing cryogenic fuel in a motor vehicle and method for using same
AU2003203277B2 (en)*2002-04-082008-08-14Whirlpool CorporationVacuum insulated refrigerator cabinet and method for evacuating the gas-tight insulated wall thereof
US6955196B2 (en)2002-04-082005-10-18Whirlpool CorporationVacuum insulated refrigerator cabinet and method for evacuating the gas-tight insulated wall thereof
EP1353135A1 (en)*2002-04-082003-10-15Whirlpool CorporationVacuum insulated refrigerator cabinet and method for evacuating the gas-tight insulated wall thereof
US20030197017A1 (en)*2002-04-082003-10-23Giorgio GiudiciVacuum insulated refrigerator cabinet and method for evacuating the gas-tight insulated wall thereof
JP4815129B2 (en)*2002-09-272011-11-16ザ リージェンツ オブ ザ ユニバーシティ オブ カリフォルニア Lightweight low temperature compatible pressure vessel for vehicle fuel storage
JP2006500536A (en)*2002-09-272006-01-05ザ リージェンツ オブ ザ ユニバーシティ オブ カリフォルニア Lightweight low temperature compatible pressure vessel for vehicle fuel storage
WO2004029503A3 (en)*2002-09-272004-07-15Univ CaliforniaLightweight cryogenic-compatible pressure vessels for vehicular fuel storage
US20090283176A1 (en)*2008-05-162009-11-19Berry Gene DCryogenic Capable High Pressure Containers for Compact Storage of Hydrogen Onboard Vehicles
US20100133279A1 (en)*2008-05-162010-06-03Berry Gene DCryogenic Capable High Pressure Containers For Compact Storage Of Hydrogen Onboard Vehicles
US20150300571A1 (en)*2014-04-162015-10-22Bayerische Motoren Werke AktiengesellschaftMethod for Producing a Tank, In Particular a Motor Vehicle Tank
US9879826B2 (en)*2014-04-162018-01-30Bayerische Motoren Werke AktiengesellschaftMethod for producing a tank, in particular a motor vehicle tank
US10794536B2 (en)2017-11-302020-10-06Cryogenic Fuels Inc.Vacuum acquisition systems and methods

Similar Documents

PublicationPublication DateTitle
US3130561A (en)Insulation device
US3485054A (en)Rapid pump-down vacuum chambers incorporating cryopumps
US4606196A (en)Vacuum insulation system
US3668881A (en)Adsorptive cryopumping method and apparatus
US2756765A (en)System for maintaining liquid level
US2677938A (en)Vacuum-insulated container and process for evacuating same
US4667390A (en)Vacuum insulation system method of manufacture
US2985356A (en)Pumping device
EP1353135B1 (en)Vacuum insulated refrigerator cabinet and method for evacuating the gas-tight insulated wall thereof
US2998708A (en)Container for low temperature liquids
US3116764A (en)High vacuum method and apparatus
US3525229A (en)On-off thermal switch for a cryopump
US4038060A (en)Apparatus for treating an exhaust gas from nuclear plant
WO1993025842A1 (en)Process for evacuating a thermally insulating jacket in particular the jacket of a dewar or of another cryogenic device
US3811794A (en)Ultrahigh vacuum sublimation pump
JPS59225275A (en)Vacuum heat-insulating material
US3464223A (en)Trap pump for vacuum system
US4704068A (en)Process for introducing an adsorption agent
JPH0278281A (en)Cryostat provided with adsorber
US4364235A (en)Helium-cooled cold surface, especially for a cryopump
BannockMolecular sieve pumping
SU842332A1 (en)Method of evacuating heat insulation cavity of cryogenic pipelines and vessels
US3348386A (en)Apparatus and method for pumping and storing gases
US2360491A (en)Water cooler
US3156406A (en)High vacuum pumping method and apparatus

[8]ページ先頭

©2009-2025 Movatter.jp