DE69002281D1 - COMBUSTION CHAMBER FOR PISTON ENGINE. - Google Patents

COMBUSTION CHAMBER FOR PISTON ENGINE.

Info

Publication number
DE69002281D1
DE69002281D1 DE9090401425T DE69002281T DE69002281D1 DE 69002281 D1 DE69002281 D1 DE 69002281D1 DE 9090401425 T DE9090401425 T DE 9090401425T DE 69002281 T DE69002281 T DE 69002281T DE 69002281 D1 DE69002281 D1 DE 69002281D1
Authority
DE
Germany
Prior art keywords
combustion chamber
piston engine
piston
engine
combustion
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
DE9090401425T
Other languages
German (de)
Other versions
DE69002281T2 (en
Inventor
Philippe H Ramette
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 (S E P) SURESNES FR S A 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 (S E P) SURESNES FR S A Ste, Societe Europeenne de Propulsion SEP SA filed Critical EUROPEENNE DE PROPULSION (S E P) SURESNES FR S A Ste
Publication of DE69002281D1 publication Critical patent/DE69002281D1/en
Application granted granted Critical
Publication of DE69002281T2 publication Critical patent/DE69002281T2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
DE1990602281 1989-05-29 1990-05-29 Combustion chamber for ramjet engine. Expired - Fee Related DE69002281T2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8907019A FR2647533B1 (en) 1989-05-29 1989-05-29 SUPERSONIC COMBUSTION STATOREACTOR CHAMBER

Publications (2)

Publication Number Publication Date
DE69002281D1 true DE69002281D1 (en) 1993-08-26
DE69002281T2 DE69002281T2 (en) 1994-01-27

Family

ID=9382105

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1990602281 Expired - Fee Related DE69002281T2 (en) 1989-05-29 1990-05-29 Combustion chamber for ramjet engine.

Country Status (4)

Country Link
EP (1) EP0401107B1 (en)
JP (1) JPH0396645A (en)
DE (1) DE69002281T2 (en)
FR (1) FR2647533B1 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19730674A1 (en) * 1997-07-17 1999-01-21 Deutsch Zentr Luft & Raumfahrt Combustion chamber and method of manufacturing a combustion chamber
JP4522558B2 (en) * 2000-08-11 2010-08-11 実 屋我 Method and apparatus for promoting fuel mixing for a scramjet engine
FR2836698B1 (en) 2002-03-04 2005-02-11 Eads Launch Vehicles COMBUSTION CHAMBER FOR STATOREACTOR AND STATOREACTOR PROVIDED WITH SUCH A COMBUSTION CHAMBER
FR2836699B1 (en) * 2002-03-04 2005-02-11 Eads Launch Vehicles ENGINE OF ROCKET
CN103343983B (en) * 2013-07-31 2014-12-24 哈尔滨工业大学 Supersonic-speed stable combustion method based on strong magnetic field stable electric arc
GB2518211B (en) * 2013-09-13 2015-11-18 Carolyn Billie Knight Rocket motor with combustion chamber having porous membrane
CN108317541B (en) * 2018-02-26 2020-07-07 中国科学院力学研究所 Ramjet engine
CN113530709B (en) * 2021-09-16 2021-12-14 西安空天引擎科技有限公司 Bimodal hydrogen peroxide gas generator

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE253189C (en) *
US2658332A (en) * 1951-03-21 1953-11-10 Carborundum Co Fluid cooled, refractory, ceramic lined rocket structure
US3114961A (en) * 1959-03-20 1963-12-24 Power Jets Res & Dev Ltd Treatment of porous bodies
GB1046909A (en) * 1963-08-26 1966-10-26 Gur Charan Saini Rocket thrust chambers
CH427118A (en) * 1963-11-28 1966-12-31 Bbc Brown Boveri & Cie Method for protecting surface parts of a heat-resistant body that is swept by hot media
BE790956A (en) * 1971-11-05 1973-03-01 Penny Robert N FLAME TUBE FOR AGAZ TURBINE ENGINE COMBUSTION CHAMBER
US3864907A (en) * 1973-11-05 1975-02-11 Us Air Force Step cylinder combustor design
FR2461690B1 (en) * 1979-07-19 1985-08-16 Europ Propulsion HIGH TEMPERATURE THERMAL INSULATION MATERIAL AND MANUFACTURING METHOD THEREOF
GB2089434A (en) * 1980-12-09 1982-06-23 Rolls Royce Composite Ducts for Jet Pipes
FR2610044A1 (en) * 1986-10-14 1988-07-29 Gen Electric PROPULSION SYSTEM COMPRISING AN IMPROVED TRIM OF THE COMBUSTION CHAMBER AND METHOD OF MANUFACTURING SUCH MANUFACTURE

Also Published As

Publication number Publication date
JPH0396645A (en) 1991-04-22
EP0401107B1 (en) 1993-07-21
EP0401107A1 (en) 1990-12-05
FR2647533A1 (en) 1990-11-30
FR2647533B1 (en) 1993-03-19
DE69002281T2 (en) 1994-01-27

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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