FR2634005B1 - Ensemble injecteur de carburant de pilotage pour un statoreacteur supersonique - Google Patents

Ensemble injecteur de carburant de pilotage pour un statoreacteur supersonique

Info

Publication number
FR2634005B1
FR2634005B1 FR888809406A FR8809406A FR2634005B1 FR 2634005 B1 FR2634005 B1 FR 2634005B1 FR 888809406 A FR888809406 A FR 888809406A FR 8809406 A FR8809406 A FR 8809406A FR 2634005 B1 FR2634005 B1 FR 2634005B1
Authority
FR
France
Prior art keywords
statoreactor
supersonic
fuel injector
pilot fuel
injector assembly
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 - Fee Related
Application number
FR888809406A
Other languages
English (en)
Other versions
FR2634005A1 (fr
Inventor
Roy N Guile
William T Peschke
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of FR2634005A1 publication Critical patent/FR2634005A1/fr
Application granted granted Critical
Publication of FR2634005B1 publication Critical patent/FR2634005B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • 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)
  • Fuel-Injection Apparatus (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR888809406A 1987-05-05 1988-07-11 Ensemble injecteur de carburant de pilotage pour un statoreacteur supersonique Expired - Fee Related FR2634005B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/046,072 US4821512A (en) 1987-05-05 1987-05-05 Piloting igniter for supersonic combustor

Publications (2)

Publication Number Publication Date
FR2634005A1 FR2634005A1 (fr) 1990-01-12
FR2634005B1 true FR2634005B1 (fr) 1993-01-29

Family

ID=21941444

Family Applications (1)

Application Number Title Priority Date Filing Date
FR888809406A Expired - Fee Related FR2634005B1 (fr) 1987-05-05 1988-07-11 Ensemble injecteur de carburant de pilotage pour un statoreacteur supersonique

Country Status (7)

Country Link
US (1) US4821512A (fr)
JP (1) JPH0674772B2 (fr)
KR (1) KR890701887A (fr)
DE (1) DE3890359C2 (fr)
FR (1) FR2634005B1 (fr)
GB (1) GB2211595B (fr)
WO (1) WO1988008927A1 (fr)

Families Citing this family (49)

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US4986068A (en) * 1988-09-16 1991-01-22 General Electric Company Hypersonic scramjet engine fuel injector
US4903480A (en) * 1988-09-16 1990-02-27 General Electric Company Hypersonic scramjet engine fuel injector
US4969327A (en) * 1988-09-16 1990-11-13 General Electric Company Hypersonic scramjet engine fuel injector
US4951463A (en) * 1988-09-16 1990-08-28 General Electric Company Hypersonic scramjet engine fuel injector
US5109670A (en) * 1989-03-23 1992-05-05 General Electric Company Scramjet combustor
US5081831A (en) * 1989-03-23 1992-01-21 General Electric Company Scramjet combustor
US5097663A (en) * 1989-03-23 1992-03-24 General Electric Company Scramjet combustor
US5072581A (en) * 1989-03-23 1991-12-17 General Electric Company Scramjet combustor
US5103633A (en) * 1989-03-23 1992-04-14 General Electric Company Scramjet combustor
US5202525A (en) * 1990-01-29 1993-04-13 General Electric Company Scramjet engine having improved fuel/air mixing
US5058826A (en) * 1990-01-29 1991-10-22 General Electric Company Scramjet engine having a low pressure combustion cycle
US5085048A (en) * 1990-02-28 1992-02-04 General Electric Company Scramjet including integrated inlet and combustor
US5255513A (en) * 1990-02-28 1993-10-26 General Electric Company Method of operating a scramjet including integrated inlet and combustor
FR2678714B1 (fr) * 1991-07-03 1993-09-17 Snecma Foyer de statoreacteur a pollution reduite.
US5174524A (en) * 1991-10-10 1992-12-29 General Electric Company Cooling system for high speed aircraft
US5280705A (en) * 1992-06-22 1994-01-25 General Electric Company Fuel injection system for scramjet engines
US5372005A (en) 1992-09-14 1994-12-13 Lawler; Shawn P. Method and apparatus for power generation
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
US5317866A (en) * 1992-09-18 1994-06-07 Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of National Defence Of Her Majesty's Canadian Government Free-flying tubular vehicle
DE4417538A1 (de) * 1994-05-19 1995-11-23 Abb Management Ag Brennkammer mit Selbstzündung
US5660040A (en) * 1994-12-20 1997-08-26 United Technologies Corporation Scramjet fuel injection system having independent fuel supplies for supersonic and hypersonic operation
DE4446611A1 (de) * 1994-12-24 1996-06-27 Abb Management Ag Brennkammer
DE4446541A1 (de) * 1994-12-24 1996-06-27 Abb Management Ag Brennkammer
FR2745605B1 (fr) * 1996-03-01 1998-04-30 Aerospatiale Dispositif d'injection de combustible pour statoreacteur d'aeronef
FR2750170B1 (fr) * 1996-06-24 1998-08-21 Aerospatiale Mat d'injection de combustible pour statoreacteur fonctionnant a un nombre de mach eleve
FR2750169B1 (fr) * 1996-06-24 1998-08-21 Aerospatiale Dispositif d'injection de combustible pour statoreacteur fonctionnant a un nombre de mach eleve
RU2101536C1 (ru) * 1996-10-17 1998-01-10 Йелстаун Корпорейшн Н.В. Способ разгона сверхзвукового прямоточного воздушно-реактивного двигателя
NZ336117A (en) 1996-12-16 2001-02-23 Ramgen Power Systems Inc Ramjet engine for power generation
ZA993917B (en) 1998-06-17 2000-01-10 Ramgen Power Systems Inc Ramjet engine for power generation.
JP2003035417A (ja) * 2001-07-24 2003-02-07 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器のパイロットノズル
US6968694B2 (en) * 2003-03-13 2005-11-29 United Technologies Corporation Augmentor
US8641411B2 (en) * 2004-01-13 2014-02-04 Faureua Emissions Control Technologies, USA, LLC Method and apparatus for directing exhaust gas through a fuel-fired burner of an emission abatement assembly
US20080196414A1 (en) * 2005-03-22 2008-08-21 Andreadis Dean E Strut cavity pilot and fuel injector assembly
WO2007067085A1 (fr) * 2005-12-06 2007-06-14 Siemens Aktiengesellschaft Procédé et appareil de combustion d’un carburant
JP4776697B2 (ja) * 2006-02-28 2011-09-21 シーメンス アクチエンゲゼルシヤフト ガスタービン用燃焼器およびガスタービン用燃焼器の運転方法
US8272221B2 (en) 2007-12-05 2012-09-25 Sharpe Thomas H Hydrogen gas generator for jet engines
US8250854B2 (en) * 2007-12-05 2012-08-28 Sharpe Thomas H Self-starting turbineless jet engine
CN100591996C (zh) * 2008-03-17 2010-02-24 中国科学院力学研究所 一种用于超声速燃烧室的壁面凹槽
ES2727703T3 (es) * 2008-10-23 2019-10-18 Mbda Uk Ltd Método y sistema para alterar la geometría de admisión de aire de un propulsor
EP2743588A1 (fr) 2012-12-11 2014-06-18 Siemens Aktiengesellschaft Positionnement d'injecteur de carburant en retrait
JP6258101B2 (ja) * 2014-03-28 2018-01-10 三菱重工業株式会社 ジェットエンジン、飛しょう体及びジェットエンジンの動作方法
RU178988U1 (ru) * 2017-09-21 2018-04-24 Общество с ограниченной ответственностью "ВНХ-Механика" Сверхзвуковой прямоточный воздушно-реактивный двигатель
US11486579B2 (en) 2018-02-26 2022-11-01 General Electric Company Engine with rotating detonation combustion system
US11320147B2 (en) 2018-02-26 2022-05-03 General Electric Company Engine with rotating detonation combustion system
US11473780B2 (en) 2018-02-26 2022-10-18 General Electric Company Engine with rotating detonation combustion system
US20190264918A1 (en) * 2018-02-26 2019-08-29 General Electric Company Engine With Rotating Detonation Combustion System
US11415080B2 (en) * 2018-05-14 2022-08-16 General Electric Company Engine for an aircraft
CN110821711B (zh) * 2019-11-07 2020-10-16 西安航天动力研究所 一种燃烧室的点火、稳燃结构
CN113236424B (zh) * 2021-06-22 2022-07-05 西安航天动力研究所 一种双下侧后置超声速进气道

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2400445A (en) * 1944-02-11 1946-05-14 Hartwell F Tucker Supporting rack for toothbrushes
US2420445A (en) * 1945-12-26 1947-05-13 Rizzuto Charles Type bar releasing device for typewriters
GB684670A (en) * 1947-10-21 1952-12-24 Power Jets Res & Dev Ltd Improvements in or relating to combustion apparatus
US2692480A (en) * 1948-05-07 1954-10-26 Onera (Off Nat Aerospatiale) Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines
US2984979A (en) * 1951-03-27 1961-05-23 Eldon R Babcock Vortex pilot flame source for ramjet engines
US2744384A (en) * 1952-08-09 1956-05-08 United Aircraft Corp Burner construction for high velocity gases
US2920445A (en) * 1957-01-15 1960-01-12 Curtiss Wright Corp Flame holder apparatus
US3075353A (en) * 1959-08-19 1963-01-29 Gen Electric Supersonic combustion
US2978868A (en) * 1959-12-21 1961-04-11 Gen Electric Concentric combustion system with cooled dividing partition
US3831375A (en) * 1967-04-07 1974-08-27 United Aircraft Corp Piloting flameholder for jet engine
US3974648A (en) * 1968-08-19 1976-08-17 United Technologies Corporation Variable geometry ramjet engine
US3864907A (en) * 1973-11-05 1975-02-11 Us Air Force Step cylinder combustor design
US4707982A (en) * 1981-06-26 1987-11-24 Rockwell International Corporation Thermal regenerative injector

Also Published As

Publication number Publication date
KR890701887A (ko) 1989-12-22
US4821512A (en) 1989-04-18
GB8829882D0 (en) 1989-03-08
JPH0674772B2 (ja) 1994-09-21
WO1988008927A1 (fr) 1988-11-17
FR2634005A1 (fr) 1990-01-12
JPH01503161A (ja) 1989-10-26
DE3890359C2 (de) 1997-09-11
GB2211595A (en) 1989-07-05
GB2211595B (en) 1991-01-02

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Legal Events

Date Code Title Description
ST Notification of lapse