US5548962A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Refueling process for cryogenic liquids
Assignee: Airbus Defence and Space GmbH
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Filing: 1995-03-01
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Granted: 1996-08-27
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Expires: 2015-03-01
Abstract
Abstract A refueling process for cryogenic liquids, in which the cryogenic liquid in question is transferred from a storage tank into a receiving tank via a detachable line connection. Before or during the refueling process, the cryogenic liquid is cooled in the storage tank to a temperature that is below the lowest operating temperature intended in the tank and above the freezing point of the liquid. The cryogenic liquid is transferred into the tank through a filter with a fineness of 5 to 40 μm, and its temperature is increased during the transfer to a value that at least approximately corresponds to the intended operating temperature in the receiving tank.
Inventors
- 👤 Peter Luger
- 👤 Franz Grafwalliner
- 👤 Helmuth Peller
- 👤 Martin Muller
- 👤 Valentin V. Malyshev
- 👤 Viacheslav P. Logviniouk
- 👤 Vladmimir S. Ozeretskovsky
- 👤 Alexander S. Shengardt
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 20:20
CPC Classifications
F; F17; F17C; F17C9/00; F17C6/00; F17C2205/00; F17C2205/01; F17C2205/0153; F17C2205/0157; F17C2205/03; F17C2205/0302; F17C2205/0341; F17C2221/00; F17C2221/01; F17C2221/012; F17C2221/03; F17C2221/032; F17C2221/033; F17C2223/00; F17C2223/01; F17C2223/0146; F17C2223/0153; F17C2223/0161; F17C2225/00; F17C2225/01; F17C2225/0146; F17C2225/0153; F17C2225/0161; F17C2227/00; F17C2227/03; F17C2227/0337; F17C2260/00; F17C2260/03; F17C2260/031; F17C2265/00; F17C2265/06; F17C2265/065; F17C2270/00; F17C2270/01; F17C2270/0186; F17C2270/0189; Y; Y02; Y02E; Y02E60/00; Y02E60/30; Y02E60/32; Y10; Y10S; Y10S62/00; Y10S62/902; Y10S62/908
Claims Analysis
Total Claims: 17
Claim 1
Independent Claim
146 words
A refueling process for cryogenic liquids, including hydrogen or liquid natural gas, for use as fuel, including transfer of cryogenic liquid from a storage tank to a receiving tank via a least one detachable line connection, the process comprising the steps of: cooling the cryogenic liquid in the storage tank, prior to transfer of the cryogenic liquid, to a temperature that is below the lowest operating temperature intended for said receiving tank and is higher than the freezing point of said cryogenic liquid; and transferring the cryogenic liquid into the receiving tank through at least one filter, the filter being provided with a fineness of 5 to 40 μm for retaining crystals of foreign gas, and the temperature of said cryogenic liquid is increased during transfer from said storage tank to said receiving tank to substantially correspond to said intended operating temperature of said receiving tank.
Claim 2
Dependent Claim
146 words
A refueling process for cryogenic liquids, including hydrogen or liquid natural gas, for use as fuel, including transfer of cryogenic liquid from a storage tank to a receiving tank via a least one detachable line connection, the process comprising the steps of: cooling the cryogenic liquid in the storage tank, prior to transfer of the cryogenic liquid, to a temperature that is below the lowest operating temperature intended for said receiving tank and is higher than the freezing point of said cryogenic liquid; and transferring the cryogenic liquid into the receiving tank through at least one filter, the filter being provided with a fineness of 5 to 40 μm for retaining crystals of foreign gas, and the temperature of said cryogenic liquid is increased during transfer from said storage tank to said receiving tank to substantially correspond to said intended operating temperature of said receiving tank.
Claim 3
Dependent Claim
29 words
A refueling process according to claim 1, wherein said step of cooling said cryogenic liquid includes cooling said cryogenic liquid in said storage tank during said step of transferring.
Claim 4
Dependent Claim
29 words
A refueling process according to claim 1, wherein said step of cooling includes cooling said cryogenic liquid at least up to a time just before said step of transferring.
Claim 5
Dependent Claim
148 words
A refueling process for cryogenic liquids, including hydrogen or liquid natural gas for use as aircraft fuel, including transfer of cryogenic liquid from a refueling tank to a aircraft tank via a least one detachable line connection, the process comprising the steps of: cooling the cryogenic liquid in the refueling tank, prior to transfer of the cryogenic liquid, to a temperature that is below the lowest operating temperature intended for said aircraft tank and is higher than the freezing point of said cryogenic liquid; and transferring the cryogenic liquid into the aircraft tank through at least one filter, the filter being provided with a fineness of 5 to 40 μm for retaining any crystals of foreign gas, and the temperature of said cryogenic liquid is increased during transfer from said refueling tank to said aircraft tank to substantially correspond to said intended operating temperature of said aircraft tank.
Claim 6
Dependent Claim
148 words
A refueling process for cryogenic liquids, including hydrogen or liquid natural gas for use as aircraft fuel, including transfer of cryogenic liquid from a refueling tank to a aircraft tank via a least one detachable line connection, the process comprising the steps of: cooling the cryogenic liquid in the refueling tank, prior to transfer of the cryogenic liquid, to a temperature that is below the lowest operating temperature intended for said aircraft tank and is higher than the freezing point of said cryogenic liquid; and transferring the cryogenic liquid into the aircraft tank through at least one filter, the filter being provided with a fineness of 5 to 40 μm for retaining any crystals of foreign gas, and the temperature of said cryogenic liquid is increased during transfer from said refueling tank to said aircraft tank to substantially correspond to said intended operating temperature of said aircraft tank.
Claim 7
Independent Claim
114 words
A method for reducing foreign gas crystallization in a user tank caused by refueling, the method comprising the steps of: providing a storage tank containing cryogenic liquid; providing a user tank capable of receiving cryogenic liquid; connecting said storage tank to said user tank for communication of the cryogenic liquid from said storage tank to said user tank; determining a minimum operating temperature of said user tank; transferring the cryogenic liquid from said storage tank to said user tank; blocking crystals of foreign gases present in the cryogenic liquid of said storage tank, which crystals of foreign gases crystalize in said user tank above said minimum operating temperature, from flowing into said user tank.
Claim 8
Independent Claim
114 words
A method for reducing foreign gas crystallization in a user tank caused by refueling, the method comprising the steps of: providing a storage tank containing cryogenic liquid; providing a user tank capable of receiving cryogenic liquid; connecting said storage tank to said user tank for communication of the cryogenic liquid from said storage tank to said user tank; determining a minimum operating temperature of said user tank; transferring the cryogenic liquid from said storage tank to said user tank; blocking crystals of foreign gases present in the cryogenic liquid of said storage tank, which crystals of foreign gases crystalize in said user tank above said minimum operating temperature, from flowing into said user tank.
Claim 9
Dependent Claim
49 words
A method in accordance with claim 5, wherein: said blocking of said foreign gases is performed by crystallizing said foreign gases present in the cryogenic liquid of said storage tank into foreign gas crystals and filtering said foreign gas crystals from the cryogenic liquid transferred to said user tank.
Claim 10
Dependent Claim
33 words
A method in accordance with claim 6, wherein: said crystallizing is performed by maintaining the cryogenic liquid at a refueling temperature during said filtering, said refueling temperature being below said minimum operating temperature.
Claim 11
Dependent Claim
17 words
A method in accordance with claim 7, wherein: said cryogenic liquid is cooled to said refueling temperature.
Claim 12
Dependent Claim
20 words
A method in accordance with claim 7, wherein: said cryogenic liquid is cooled in said storage tank during said transferring.
Claim 13
Dependent Claim
18 words
A method in accordance with claim 7, wherein: said cryogenic liquid is cooled before and until said transferring.
Claim 14
Dependent Claim
20 words
A method in accordance with claim 7, wherein: said refueling temperature is above a freezing point of the cryogenic fluid.
Claim 15
Dependent Claim
21 words
A method in accordance with claim 7, further comprising: heating the cryogenic fluid after said filtering to said minimum operating temperature.
Claim 16
Dependent Claim
20 words
A method in accordance with claim 6, wherein: said filtering uses filters having a fineness of 5 to 40 μm.
Claim 17
Dependent Claim
25 words
A method in accordance with claim 5, further comprising: storing the cryogenic liquid in said storage tank at a temperature above said minimum operating temperature.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1999-08-27 | 2000-02-26 | 2000-08-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2003-08-27 | 2004-02-26 | 2004-08-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2007-08-27 | 2008-02-26 | 2008-08-27 | $7700.00 | Window Closed / Lapsed |