DE2413507A1 - Gasturbine fuer kryogenen kraftstoff - Google Patents

Gasturbine fuer kryogenen kraftstoff

Info

Publication number
DE2413507A1
DE2413507A1 DE2413507A DE2413507A DE2413507A1 DE 2413507 A1 DE2413507 A1 DE 2413507A1 DE 2413507 A DE2413507 A DE 2413507A DE 2413507 A DE2413507 A DE 2413507A DE 2413507 A1 DE2413507 A1 DE 2413507A1
Authority
DE
Germany
Prior art keywords
hydrogen
gas turbine
compressor
combustion chamber
turbine according
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.)
Pending
Application number
DE2413507A
Other languages
German (de)
English (en)
Inventor
Hermann Dr Hagen
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Priority to DE2413507A priority Critical patent/DE2413507A1/de
Priority to US05/556,502 priority patent/US4062184A/en
Priority to FR7508783A priority patent/FR2264973B3/fr
Priority to GB11632/75A priority patent/GB1499205A/en
Publication of DE2413507A1 publication Critical patent/DE2413507A1/de
Pending 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
    • 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
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
DE2413507A 1974-03-20 1974-03-20 Gasturbine fuer kryogenen kraftstoff Pending DE2413507A1 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE2413507A DE2413507A1 (de) 1974-03-20 1974-03-20 Gasturbine fuer kryogenen kraftstoff
US05/556,502 US4062184A (en) 1974-03-20 1975-03-07 Cryogenic fuel evaporation in compressor of gas turbine
FR7508783A FR2264973B3 (https=) 1974-03-20 1975-03-20
GB11632/75A GB1499205A (en) 1974-03-20 1975-03-20 Gas turbine for cryogenic fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2413507A DE2413507A1 (de) 1974-03-20 1974-03-20 Gasturbine fuer kryogenen kraftstoff

Publications (1)

Publication Number Publication Date
DE2413507A1 true DE2413507A1 (de) 1975-10-02

Family

ID=5910680

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2413507A Pending DE2413507A1 (de) 1974-03-20 1974-03-20 Gasturbine fuer kryogenen kraftstoff

Country Status (4)

Country Link
US (1) US4062184A (https=)
DE (1) DE2413507A1 (https=)
FR (1) FR2264973B3 (https=)
GB (1) GB1499205A (https=)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3139118A1 (fr) * 2022-08-30 2024-03-01 Airbus Operations Ensemble propulsif pour aéronef
FR3139119A1 (fr) * 2022-08-30 2024-03-01 Airbus Operations Ensemble propulsif pour aéronef
EP4345010A1 (fr) 2022-09-30 2024-04-03 Airbus Ensemble propulsif pour aéronef
EP4345009A1 (fr) 2022-09-30 2024-04-03 Airbus Ensemble propulsif pour aéronef
FR3145746A1 (fr) * 2023-02-14 2024-08-16 Airbus Operations Ensemble propulsif pour aéronef

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GB2126658B (en) * 1982-09-07 1986-07-02 Secr Defence Generation of power from liquid hydrogen
EP0561011A1 (de) * 1992-03-16 1993-09-22 Asea Brown Boveri Ag Zwischengekühlte Verdichter
US5697207A (en) * 1996-08-02 1997-12-16 General Electric Co. Combined gas turbine inlet chiller, nox control device and power augmentation system and methods of operation
GB9701416D0 (en) * 1997-01-24 1997-03-12 Boc Group Plc An air compressor
US6192668B1 (en) 1999-10-19 2001-02-27 Capstone Turbine Corporation Method and apparatus for compressing gaseous fuel in a turbine engine
US20020166324A1 (en) 1998-04-02 2002-11-14 Capstone Turbine Corporation Integrated turbine power generation system having low pressure supplemental catalytic reactor
US6907735B2 (en) * 2002-08-27 2005-06-21 Proton Energy Systems, Inc. Hydrogen fueled electrical generator system and method thereof
RU2353787C1 (ru) * 2007-09-06 2009-04-27 Открытое акционерное общество "Российские железные дороги" (ОАО "РЖД") Газотурбинная установка
US20100083940A1 (en) * 2008-10-04 2010-04-08 Woodford Leon Vrazel Cryogenic air cooler for improving power and fuel efficiency of a motor vehicle internal combustion engine
GB2479001A (en) * 2010-03-26 2011-09-28 Linde Ag Compressor with atomised cryogenic liquefied gas injection
US20130186059A1 (en) * 2010-09-30 2013-07-25 General Electric Company Dual fuel aircraft system and method for operating same
RU2474718C2 (ru) * 2011-01-25 2013-02-10 Николай Евгеньевич Староверов Способ форсажа турбодвигателя и двигатель для его реализации (варианты)
WO2013188956A1 (en) * 2012-06-20 2013-12-27 Daniel Pomerleau Cryogenic fuel combustion engines
CA2891549A1 (en) * 2012-11-30 2014-08-28 General Electric Company Dual fuel aircraft system comprising a thermostatic expansion valve
CA2896463A1 (en) * 2012-12-28 2014-07-03 General Electric Company Turbine engine assembly comprising a cryogenic fuel system
BR112015023299A2 (pt) * 2013-03-15 2017-07-18 Gen Electric método de uso de combustível criogênico e sistema de vaporização de combustível
RU2568031C2 (ru) * 2014-01-17 2015-11-10 Николай Евгеньевич Староверов Способ форсажа турбодвигателя-2
US10119496B2 (en) 2014-04-15 2018-11-06 Cummins Inc. Cryogenic fuel injection and combustion
RU2578941C2 (ru) * 2014-07-15 2016-03-27 Владимир Леонидович Письменный Способ форсирования двухконтурного турбореактивного двигателя
US11434823B2 (en) * 2020-01-06 2022-09-06 Raytheon Technologies Corporation Systems and methods for power transfer in cryogenic fuel applications
US20210340908A1 (en) 2020-05-01 2021-11-04 Raytheon Technologies Corporation Gas turbine engines having cryogenic fuel systems
RU2746082C1 (ru) * 2020-09-15 2021-04-06 Владимир Александрович Шишков Система регулирования газотурбинного двигателя
FR3120114A1 (fr) * 2021-02-25 2022-08-26 Airbus Operations Aéronef comportant un moteur et un système de refroidissement à base de dihydrogène
US12241424B2 (en) * 2021-03-23 2025-03-04 General Electric Company Hydrogen fuel leak detection system
US11542869B2 (en) * 2021-05-27 2023-01-03 Pratt & Whitney Canada Corp. Dual cycle intercooled hydrogen engine architecture
US11761381B2 (en) * 2021-08-14 2023-09-19 Pratt & Whitney Canada Corp. Gas turbine engine comprising liquid hydrogen evaporators and heaters
FR3129661A1 (fr) * 2021-11-29 2023-06-02 Airbus Systeme de chauffage de dihydrogene et de refroidissement de fluide combines pour aeronef, et aeronef comprenant un tel systeme
US20230323814A1 (en) * 2022-04-08 2023-10-12 Raytheon Technologies Corporation Hydrogen turbine power assisted condensation
US12473862B2 (en) 2022-05-13 2025-11-18 General Electric Company Purge system for a hydrogen fuel system
US12428991B2 (en) * 2022-05-19 2025-09-30 Rtx Corporation Reverse flow hydrogen steam injected turbine engine
US20240141831A1 (en) * 2022-05-19 2024-05-02 Raytheon Technologies Corporation Hydrogen steam injected turbine engine with cooled cooling air
CN114876645B (zh) * 2022-06-10 2023-11-03 贾煊 一种双燃料节能环保航空发动机
US12152532B2 (en) * 2023-01-27 2024-11-26 Rtx Corporation Split evaporator for steam injection turbine engine
US12180893B2 (en) * 2023-01-27 2024-12-31 Rtx Corporation Hydrogen steam injected turbine engine with turboexpander heat recovery
US20240426242A1 (en) * 2023-06-23 2024-12-26 Raytheon Technologies Corporation Cryogenic air separation enhanced gas turbine
FR3151299B1 (fr) 2023-07-20 2025-08-01 Airbus Operations Sas Ensemble propulsif pour aéronef
US20250163850A1 (en) * 2023-11-21 2025-05-22 General Electric Company Turbine engine including a steam system

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US2602289A (en) * 1945-05-25 1952-07-08 Rateau Soc Method and means for propelling a vehicle using normally gaseous fuel as a liquid
US2630678A (en) * 1947-08-18 1953-03-10 United Aircraft Corp Gas turbine power plant with fuel injection between compressor stages
US2689452A (en) * 1949-12-02 1954-09-21 United Aircraft Corp Device for increasing the thrust of turbojet engines
US2718753A (en) * 1951-01-02 1955-09-27 Phillips Petroleum Co Improved operation of internal combustion engine operating on liquid petroleum gas fuel
US2977756A (en) * 1956-03-26 1961-04-04 Gen Motors Corp Fuel control for a turbo-prop engine using operating limits of power output temperature
US2907527A (en) * 1956-04-10 1959-10-06 Thompson Ramo Wooldridge Inc Nozzle
US2952974A (en) * 1958-09-03 1960-09-20 Chandler Evans Corp Temperature control apparatus for turbojet engine
US3263421A (en) * 1963-12-18 1966-08-02 Holley Carburetor Co Fuel control system for igniter and main burner of gas turbine engine
US3313103A (en) * 1965-08-25 1967-04-11 Gen Motors Corp Gas turbine combustion process

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3139118A1 (fr) * 2022-08-30 2024-03-01 Airbus Operations Ensemble propulsif pour aéronef
FR3139119A1 (fr) * 2022-08-30 2024-03-01 Airbus Operations Ensemble propulsif pour aéronef
EP4332352A1 (fr) 2022-08-30 2024-03-06 Airbus Operations Ensemble propulsif pour aéronef
EP4331993A1 (fr) * 2022-08-30 2024-03-06 Airbus Operations Ensemble propulsif pour aéronef
US12398677B2 (en) 2022-08-30 2025-08-26 Airbus Operations Sas Powerplant for an aircraft
US12291350B2 (en) 2022-08-30 2025-05-06 Airbus Operations Sas Powerplant for an aircraft
FR3140352A1 (fr) * 2022-09-30 2024-04-05 Airbus Ensemble propulsif pour aéronef
FR3140351A1 (fr) * 2022-09-30 2024-04-05 Airbus Ensemble propulsif pour aéronef
US12292001B2 (en) 2022-09-30 2025-05-06 Airbus Sas Propulsive assembly for aircraft
EP4345009A1 (fr) 2022-09-30 2024-04-03 Airbus Ensemble propulsif pour aéronef
EP4345010A1 (fr) 2022-09-30 2024-04-03 Airbus Ensemble propulsif pour aéronef
FR3145746A1 (fr) * 2023-02-14 2024-08-16 Airbus Operations Ensemble propulsif pour aéronef
EP4417521A1 (fr) * 2023-02-14 2024-08-21 Airbus Operations Ensemble propulsif pour aéronef
US12338775B2 (en) 2023-02-14 2025-06-24 Airbus Operations Sas Propulsion assembly for an aircraft

Also Published As

Publication number Publication date
GB1499205A (en) 1978-01-25
FR2264973B3 (https=) 1977-11-25
US4062184A (en) 1977-12-13
FR2264973A1 (https=) 1975-10-17

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