GB899312A - Gas turbine engines - Google Patents

Gas turbine engines

Info

Publication number
GB899312A
GB899312A GB32304/59A GB3230459A GB899312A GB 899312 A GB899312 A GB 899312A GB 32304/59 A GB32304/59 A GB 32304/59A GB 3230459 A GB3230459 A GB 3230459A GB 899312 A GB899312 A GB 899312A
Authority
GB
United Kingdom
Prior art keywords
combustion
gas turbine
turbine
supporter
cryogenic fuel
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
Application number
GB32304/59A
Inventor
Arnold William Morley
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son Ltd
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
Application filed by D Napier and Son Ltd filed Critical D Napier and Son Ltd
Priority to GB32304/59A priority Critical patent/GB899312A/en
Publication of GB899312A publication Critical patent/GB899312A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/30—Fuel systems for specific fuels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells

Abstract

899,312. Gas turbine engines. NAPIER & SON Ltd., D. Sept. 13, 1960 [Sept. 22, 1959], No. 32304/59. Class 110 (3). A gas turbine engine has means for storing in liquid form a supply of cryogenic fuel or supporter of combustion for combustion in the engine in gaseous form and means for also utilizing at least some of the cryogenic fuel or supporter of combustion as an indirect coolant for the turbine. A cryogenic fuel or supporter of combustion is stated to be a substance that is gaseous at normal temperature and pressure (760 mm. Hg and 68‹ F.), but which can be stored in liquid form after refrigeration. Examples of these fuels and supporters of combustion are given as hydrogen, oxygen and fluorine and they may also be partly used as direct coolant of the turbine. A gas turbine plant has air taken from the compressor 10 which is cooled by passing through a heat exchanger 21 before being used to cool the turbine 14 driving the compressor. The heat exchanger 21 is cooled by hydrogen vapour drawn from an insulated refrigerated tank 19 by an engine driven pump 18.
GB32304/59A 1959-09-22 1959-09-22 Gas turbine engines Expired GB899312A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB32304/59A GB899312A (en) 1959-09-22 1959-09-22 Gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB32304/59A GB899312A (en) 1959-09-22 1959-09-22 Gas turbine engines

Publications (1)

Publication Number Publication Date
GB899312A true GB899312A (en) 1962-06-20

Family

ID=10336525

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32304/59A Expired GB899312A (en) 1959-09-22 1959-09-22 Gas turbine engines

Country Status (1)

Country Link
GB (1) GB899312A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4120150A (en) * 1977-05-17 1978-10-17 The United States Of America As Represented By The Secretary Of The Air Force Compact fuel-to-air heat exchanger for jet engine application
US4137705A (en) * 1977-07-25 1979-02-06 General Electric Company Cooling air cooler for a gas turbine engine
US5095693A (en) * 1989-08-04 1992-03-17 United Technologies Corporation High-efficiency gas turbine engine
EP0519304A1 (en) * 1991-06-21 1992-12-23 Siemens Aktiengesellschaft Method and device to improve a gas turbine system
FR2681641A1 (en) * 1991-09-25 1993-03-26 Mtu Muenchen Gmbh COOLING DEVICE FOR REACTION ENGINES, ESPECIALLY FOR HYPERSONIC REACTION ENGINES.
US5233823A (en) * 1989-08-04 1993-08-10 United Technologies Corporation High-efficiency gas turbine engine
WO2012045034A3 (en) * 2010-09-30 2012-07-05 General Electric Company Aircraft engine systems and methods for operating same
JP2014520231A (en) * 2011-06-17 2014-08-21 ゼネラル・エレクトリック・カンパニイ Aircraft engine fuel system and method of operating the same
CN114483307A (en) * 2022-01-21 2022-05-13 上海慕帆动力科技有限公司 Efficiency improving system and control method of hydrogen fuel gas turbine
US20230022809A1 (en) * 2021-07-22 2023-01-26 Pratt & Whitney Canada Corp. Dual cycle intercooled engine architectures
EP4129827A1 (en) 2021-08-03 2023-02-08 Airbus (S.A.S.) Aircraft including at least one device for supplying hydrogen and at least one sealed container in which is positioned at least one piece of equipment of said device for supplying hydrogen

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4120150A (en) * 1977-05-17 1978-10-17 The United States Of America As Represented By The Secretary Of The Air Force Compact fuel-to-air heat exchanger for jet engine application
US4137705A (en) * 1977-07-25 1979-02-06 General Electric Company Cooling air cooler for a gas turbine engine
US5233823A (en) * 1989-08-04 1993-08-10 United Technologies Corporation High-efficiency gas turbine engine
US5095693A (en) * 1989-08-04 1992-03-17 United Technologies Corporation High-efficiency gas turbine engine
EP0519304A1 (en) * 1991-06-21 1992-12-23 Siemens Aktiengesellschaft Method and device to improve a gas turbine system
US5272870A (en) * 1991-09-25 1993-12-28 Mtu Motoren- Und Turbinen-Union Munchen Gmbh Cooling arrangement for jet engines
FR2681641A1 (en) * 1991-09-25 1993-03-26 Mtu Muenchen Gmbh COOLING DEVICE FOR REACTION ENGINES, ESPECIALLY FOR HYPERSONIC REACTION ENGINES.
WO2012045034A3 (en) * 2010-09-30 2012-07-05 General Electric Company Aircraft engine systems and methods for operating same
JP2013543556A (en) * 2010-09-30 2013-12-05 ゼネラル・エレクトリック・カンパニイ Aircraft engine system and method for operating the same
JP2014520231A (en) * 2011-06-17 2014-08-21 ゼネラル・エレクトリック・カンパニイ Aircraft engine fuel system and method of operating the same
US20230022809A1 (en) * 2021-07-22 2023-01-26 Pratt & Whitney Canada Corp. Dual cycle intercooled engine architectures
EP4129827A1 (en) 2021-08-03 2023-02-08 Airbus (S.A.S.) Aircraft including at least one device for supplying hydrogen and at least one sealed container in which is positioned at least one piece of equipment of said device for supplying hydrogen
CN114483307A (en) * 2022-01-21 2022-05-13 上海慕帆动力科技有限公司 Efficiency improving system and control method of hydrogen fuel gas turbine
CN114483307B (en) * 2022-01-21 2023-09-26 上海慕帆动力科技有限公司 Efficiency improving system and control method of hydrogen fuel gas turbine

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