DE69308518T2 - Injektor mit einer porösen Wand für eine Raketenbrennkammer - Google Patents

Injektor mit einer porösen Wand für eine Raketenbrennkammer

Info

Publication number
DE69308518T2
DE69308518T2 DE69308518T DE69308518T DE69308518T2 DE 69308518 T2 DE69308518 T2 DE 69308518T2 DE 69308518 T DE69308518 T DE 69308518T DE 69308518 T DE69308518 T DE 69308518T DE 69308518 T2 DE69308518 T2 DE 69308518T2
Authority
DE
Germany
Prior art keywords
combustion chamber
porous wall
rocket combustion
wall injector
injector
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
DE69308518T
Other languages
English (en)
Other versions
DE69308518D1 (de
Inventor
Didier Vuillamy
Etienne Tiret
Andre Beaurain
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.)
Safran Aircraft Engines SAS
Original Assignee
EUROPEENNE DE PROPULSION SURESNES FR Ste
Societe Europeenne de Propulsion SEP SA
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 EUROPEENNE DE PROPULSION SURESNES FR Ste, Societe Europeenne de Propulsion SEP SA filed Critical EUROPEENNE DE PROPULSION SURESNES FR Ste
Publication of DE69308518D1 publication Critical patent/DE69308518D1/de
Application granted granted Critical
Publication of DE69308518T2 publication Critical patent/DE69308518T2/de
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
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors
DE69308518T 1992-12-24 1993-12-17 Injektor mit einer porösen Wand für eine Raketenbrennkammer Expired - Fee Related DE69308518T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9215719A FR2699963B1 (fr) 1992-12-24 1992-12-24 Générateur de gaz à combustion rapprochée.

Publications (2)

Publication Number Publication Date
DE69308518D1 DE69308518D1 (de) 1997-04-10
DE69308518T2 true DE69308518T2 (de) 1997-08-07

Family

ID=9437107

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69308518T Expired - Fee Related DE69308518T2 (de) 1992-12-24 1993-12-17 Injektor mit einer porösen Wand für eine Raketenbrennkammer

Country Status (5)

Country Link
US (1) US5438834A (de)
EP (1) EP0604279B1 (de)
JP (1) JPH06221560A (de)
DE (1) DE69308518T2 (de)
FR (1) FR2699963B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007063539A1 (de) * 2007-12-21 2009-06-25 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammervorrichtung
DE102010043337A1 (de) * 2010-11-03 2012-05-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Fluidzuführungsvorrichtung

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19651646C2 (de) * 1996-12-12 2002-07-11 Deutsch Zentr Luft & Raumfahrt Verfahren zum Einblasen einer ersten und zweiten Brennstoffkomponente und Einblaskopf
DE19901424B4 (de) * 1999-01-18 2009-09-10 Astrium Gmbh Brennkammer mit Transpirationskühlung
US6579085B1 (en) 2000-05-05 2003-06-17 The Boc Group, Inc. Burner and combustion method for the production of flame jet sheets in industrial furnaces
US6758386B2 (en) * 2001-09-18 2004-07-06 The Boeing Company Method of joining ceramic matrix composites and metals
FR2836698B1 (fr) 2002-03-04 2005-02-11 Eads Launch Vehicles Chambre de combustion pour statoreacteur et statoreacteur pourvu d'une telle chambre de combustion
FR2836699B1 (fr) 2002-03-04 2005-02-11 Eads Launch Vehicles Moteur de fusee
US7128532B2 (en) * 2003-07-22 2006-10-31 The Boeing Company Transpiration cooling system
US20050034446A1 (en) * 2003-08-11 2005-02-17 Fielder William Sheridan Dual capture jet turbine and steam generator
US7665307B2 (en) * 2005-12-22 2010-02-23 United Technologies Corporation Dual wall combustor liner
DE102006029586A1 (de) * 2006-06-20 2007-12-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Einblaskopf, Mischungsraum und Triebwerk
FR2933744B1 (fr) * 2008-07-11 2011-06-03 Snecma Moteur-fusee et reacteur comportant une pluralite de tels moteurs-fusees.
US8413446B2 (en) * 2008-12-10 2013-04-09 Caterpillar Inc. Fuel injector arrangement having porous premixing chamber
US20100236248A1 (en) * 2009-03-18 2010-09-23 Karthick Kaleeswaran Combustion Liner with Mixing Hole Stub
JP2011099654A (ja) * 2009-11-09 2011-05-19 Mitsubishi Heavy Ind Ltd ガスタービン用燃焼バーナ
US9341118B2 (en) 2009-12-29 2016-05-17 Rolls-Royce Corporation Various layered gas turbine engine component constructions
US9310079B2 (en) * 2010-12-30 2016-04-12 Rolls-Royce North American Technologies, Inc. Combustion liner with open cell foam and acoustic damping layers
DE102011000383B4 (de) 2011-01-28 2015-01-22 Deutsches Zentrum für Luft- und Raumfahrt e.V. Triebwerkvorrichtung und Verfahren zum Betreiben einer Triebwerkvorrichtung
FR2975442B1 (fr) * 2011-05-16 2016-08-19 Snecma Element d'injection calibrable
KR101689930B1 (ko) * 2014-09-04 2016-12-27 한국기계연구원 유동 균일성이 향상된 연소기용 연료 공급 장치
RU2640893C1 (ru) * 2016-08-19 2018-01-12 Акционерное общество "Конструкторское бюро химавтоматики" Камера сгорания жрд, работающего с дожиганием генераторного газа
JP7014632B2 (ja) * 2018-02-21 2022-02-01 川崎重工業株式会社 バーナ装置
EP3904768B1 (de) 2020-04-28 2024-04-17 Collins Engine Nozzles, Inc. Fluiddüse
CN112922744B (zh) * 2021-03-05 2023-01-06 中国空气动力研究与发展中心空天技术研究所 一种壁面嵌入式的飞行器燃料输送装置

Family Cites Families (15)

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Publication number Priority date Publication date Assignee Title
GB815596A (en) * 1955-11-11 1959-07-01 California Inst Res Found Porous metal wall construction and method of manufacture
US2405785A (en) * 1944-03-14 1946-08-13 Daniel And Florence Guggenheim Combustion chamber
US2487435A (en) * 1948-02-07 1949-11-08 Esther C Goodard Fuel and water feeding and steam discharge arrangement for combustion chambers
US2698514A (en) * 1952-01-14 1955-01-04 Edwin H Hull Rocket motor
US3623329A (en) * 1960-04-12 1971-11-30 United Aircraft Corp Control system for liquid rocket
US3242670A (en) * 1962-08-27 1966-03-29 United Aircraft Corp Segmented baffle injector design
GB1046909A (en) * 1963-08-26 1966-10-26 Gur Charan Saini Rocket thrust chambers
US4214439A (en) * 1966-05-13 1980-07-29 The United States Of America As Represented By The Secretary Of The Navy Multi component propulsion system and method
US3516254A (en) * 1967-09-11 1970-06-23 United Aircraft Corp Closed-loop rocket propellant cycle
GB1227347A (de) * 1967-10-26 1971-04-07
US3608833A (en) * 1969-10-13 1971-09-28 Aerojet General Co Fluid distributors and thrusters
BE790956A (fr) * 1971-11-05 1973-03-01 Penny Robert N Tube de flamme pour chambre de combustion de moteur a turbine agaz
JPS56138608A (en) * 1980-03-31 1981-10-29 Toshiba Corp Liquid fuel combustor
US4377067A (en) * 1980-11-24 1983-03-22 Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt Steam generator
JPS61228225A (ja) * 1985-03-30 1986-10-11 Agency Of Ind Science & Technol ガスタ−ビン用燃焼器のライナ−

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007063539A1 (de) * 2007-12-21 2009-06-25 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammervorrichtung
DE102010043337A1 (de) * 2010-11-03 2012-05-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Fluidzuführungsvorrichtung
DE102010043337B4 (de) 2010-11-03 2023-01-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Fluidzuführungsvorrichtung

Also Published As

Publication number Publication date
FR2699963B1 (fr) 1995-03-17
EP0604279A1 (de) 1994-06-29
US5438834A (en) 1995-08-08
JPH06221560A (ja) 1994-08-09
DE69308518D1 (de) 1997-04-10
EP0604279B1 (de) 1997-03-05
FR2699963A1 (fr) 1994-07-01

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MO

8339 Ceased/non-payment of the annual fee