FR2591664B1 - Systeme d'injection de carburant pour statoreacteur, statoreacteur pourvu d'un tel systeme d'injection et missile propulse par ce statoreacteur - Google Patents
Systeme d'injection de carburant pour statoreacteur, statoreacteur pourvu d'un tel systeme d'injection et missile propulse par ce statoreacteurInfo
- Publication number
- FR2591664B1 FR2591664B1 FR8518513A FR8518513A FR2591664B1 FR 2591664 B1 FR2591664 B1 FR 2591664B1 FR 8518513 A FR8518513 A FR 8518513A FR 8518513 A FR8518513 A FR 8518513A FR 2591664 B1 FR2591664 B1 FR 2591664B1
- Authority
- FR
- France
- Prior art keywords
- statoreactor
- injection system
- same
- fuel injection
- missile
- 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
Links
- 238000002347 injection Methods 0.000 title 2
- 239000007924 injection Substances 0.000 title 2
- 239000000446 fuel Substances 0.000 title 1
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
- F02K7/18—Composite ram-jet/rocket engines
-
- 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)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8518513A FR2591664B1 (fr) | 1985-12-13 | 1985-12-13 | Systeme d'injection de carburant pour statoreacteur, statoreacteur pourvu d'un tel systeme d'injection et missile propulse par ce statoreacteur |
GB8628490A GB2184225B (en) | 1985-12-13 | 1986-11-28 | Fuel injection system, ramjet engine having such an injection system, and missile propelled by said engine |
DE3642654A DE3642654C2 (de) | 1985-12-13 | 1986-12-11 | Treibstoffeinspritzsystem für Staustrahltriebwerke |
US07/210,198 US4852348A (en) | 1985-12-13 | 1988-06-20 | Fuel injection system for ramjet engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8518513A FR2591664B1 (fr) | 1985-12-13 | 1985-12-13 | Systeme d'injection de carburant pour statoreacteur, statoreacteur pourvu d'un tel systeme d'injection et missile propulse par ce statoreacteur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2591664A1 FR2591664A1 (fr) | 1987-06-19 |
FR2591664B1 true FR2591664B1 (fr) | 1988-03-25 |
Family
ID=9325773
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8518513A Expired FR2591664B1 (fr) | 1985-12-13 | 1985-12-13 | Systeme d'injection de carburant pour statoreacteur, statoreacteur pourvu d'un tel systeme d'injection et missile propulse par ce statoreacteur |
Country Status (4)
Country | Link |
---|---|
US (1) | US4852348A (fr) |
DE (1) | DE3642654C2 (fr) |
FR (1) | FR2591664B1 (fr) |
GB (1) | GB2184225B (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2629136B1 (fr) * | 1985-09-17 | 1990-11-09 | Aerospatiale | Statoreacteur pourvu d'une pluralite de manches d'alimentation en air carbure et missile pourvu d'un tel statoreacteur |
US5168698A (en) * | 1991-04-22 | 1992-12-08 | General Electric Company | Fuel manifold system for gas turbine engines |
US5386851A (en) * | 1993-06-28 | 1995-02-07 | General Electric Company | Two dimensional modulated burner staging valve |
GB9818529D0 (en) * | 1998-08-25 | 1998-10-21 | Boc Group Plc | Variable stoichiometric combustion |
FR2819556B1 (fr) * | 2001-01-12 | 2003-04-04 | Aerospatiale Matra Missiles | Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur |
DE102007010349B4 (de) * | 2007-03-03 | 2009-07-09 | Lfk-Lenkflugkörpersysteme Gmbh | Ventilsteuereinheit für Staustrahlantrieb sowie Lenkflugkörper mit einer solchen Ventilsteuereinheit |
CN102278232B (zh) * | 2011-05-26 | 2014-05-28 | 南京航空航天大学 | 改进的超燃燃烧室及其旋流器的设计方法 |
CN109540526B (zh) * | 2018-12-09 | 2021-10-15 | 西安航天动力试验技术研究所 | 一种用于冲压发动机直连试验中涡轮引射系统 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2636553A (en) * | 1949-11-08 | 1953-04-28 | Rolls Royce | Fuel system for gas turbine engines and the like with main and pilot fuel injectors |
US2716329A (en) * | 1952-08-01 | 1955-08-30 | David R Lunger | Jet engine |
FR1109645A (fr) * | 1954-08-09 | 1956-01-31 | Snecma | Propulseur à réaction destiné notamment aux engins téléguidés |
US3020717A (en) * | 1958-01-16 | 1962-02-13 | North American Aviation Inc | Uniform fuel-air ratio fuel injection system |
GB1102572A (en) * | 1964-06-06 | 1968-02-07 | Bristol Siddeley Engines Ltd | Jet propulsion engines |
US3802192A (en) * | 1972-10-04 | 1974-04-09 | Us Air Force | Integral rocket-ramjet with combustor plenum chamber |
US4327886A (en) * | 1972-11-30 | 1982-05-04 | The United States Of America As Represented By The Secretary Of The Navy | Integral rocket ramjet missile |
FR2257789A1 (en) * | 1973-07-27 | 1975-08-08 | Onera (Off Nat Aerospatiale) | Propulsive unit for missile - has jet and rocket with coaxial discharges axially displaced from each other |
US4441312A (en) * | 1979-06-22 | 1984-04-10 | The United States Of America As Represented By The Secretary Of The Air Force | Combined cycle ramjet engine |
US4539811A (en) * | 1982-01-27 | 1985-09-10 | The United States Of America As Represented By The Secretary Of The Navy | Multi-port dump combustor |
US4499735A (en) * | 1982-03-23 | 1985-02-19 | The United States Of America As Represented By The Secretary Of The Air Force | Segmented zoned fuel injection system for use with a combustor |
-
1985
- 1985-12-13 FR FR8518513A patent/FR2591664B1/fr not_active Expired
-
1986
- 1986-11-28 GB GB8628490A patent/GB2184225B/en not_active Expired
- 1986-12-11 DE DE3642654A patent/DE3642654C2/de not_active Expired - Fee Related
-
1988
- 1988-06-20 US US07/210,198 patent/US4852348A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
GB2184225A (en) | 1987-06-17 |
GB2184225B (en) | 1989-10-18 |
US4852348A (en) | 1989-08-01 |
GB8628490D0 (en) | 1987-01-07 |
DE3642654C2 (de) | 1998-11-05 |
FR2591664A1 (fr) | 1987-06-19 |
DE3642654A1 (de) | 1987-06-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
ST | Notification of lapse |