GB2068090B - Closure for ram-jets - Google Patents

Closure for ram-jets

Info

Publication number
GB2068090B
GB2068090B GB8101393A GB8101393A GB2068090B GB 2068090 B GB2068090 B GB 2068090B GB 8101393 A GB8101393 A GB 8101393A GB 8101393 A GB8101393 A GB 8101393A GB 2068090 B GB2068090 B GB 2068090B
Authority
GB
United Kingdom
Prior art keywords
jets
closure
ram
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
Application number
GB8101393A
Other versions
GB2068090A (en
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB2068090A publication Critical patent/GB2068090A/en
Application granted granted Critical
Publication of GB2068090B publication Critical patent/GB2068090B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/10Plants 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
    • F02K7/18Composite ram-jet/rocket engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • F02K9/978Closures for nozzles; Nozzles comprising ejectable or discardable elements
GB8101393A 1980-01-29 1981-01-16 Closure for ram-jets Expired GB2068090B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19803002977 DE3002977C2 (en) 1980-01-29 1980-01-29 Lid made of easily destructible material to close the air inlet openings opening into the combustion chamber of ramjet rocket engines, with a pyrotechnically functioning impact device to destroy the lid

Publications (2)

Publication Number Publication Date
GB2068090A GB2068090A (en) 1981-08-05
GB2068090B true GB2068090B (en) 1983-05-25

Family

ID=6093102

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8101393A Expired GB2068090B (en) 1980-01-29 1981-01-16 Closure for ram-jets

Country Status (3)

Country Link
DE (1) DE3002977C2 (en)
FR (1) FR2474593A1 (en)
GB (1) GB2068090B (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2584456B1 (en) * 1985-07-03 1987-10-02 Poudres & Explosifs Ste Nale DEVICE FOR TEMPORARILY CLOSING AN INTERNAL ORIFICE OF A PROPELLER
US4738099A (en) * 1986-06-09 1988-04-19 Fike Corporation Bulkhead rupture disc for solid propellant missiles
FR2863665B1 (en) * 1988-10-12 2007-03-30 Aerospatiale STATOREACTOR HAVING A TUBULAR AND MISSILE STRUCTURE PROPULATED BY SUCH STATOREACTOR
FR2755182B1 (en) * 1996-10-30 1998-12-31 Aerospatiale BLINDING SYSTEM FOR AN AIR INTAKE PORT IN THE COMBUSTION CHAMBER OF A STATOREACTOR
US5784877A (en) * 1996-11-08 1998-07-28 Atlantic Research Corporation Rocket-ramjet engine casing port closure
FR2813344B1 (en) * 2000-08-28 2002-11-29 Aerospatiale Matra Missiles BLINDING SYSTEM FOR A DUCT ORIFICE, PARTICULARLY FOR AN ORIFICE OF AN AIR INTAKE PATHWAY IN THE COMBUSTION CHAMBER OF A STATOREACTOR
CN107191291A (en) * 2017-07-13 2017-09-22 西安航天动力研究所 The dust guard and its installation method of a kind of engine
CN109488460B (en) * 2017-09-12 2021-02-19 江西洪都航空工业集团有限责任公司 Blocking cover device for supersonic air inlet

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2952972A (en) * 1957-09-09 1960-09-20 Norman A Kimmel Rocket motor and method of operating same
DE1626069B1 (en) * 1967-10-18 1970-10-08 Messerschmitt Boelkow Blohm Combination engine
GB1378079A (en) * 1972-05-22 1974-12-18 Ici Ltd Bursting disc assembly
US3901028A (en) * 1972-09-13 1975-08-26 Us Air Force Ramjet with integrated rocket boost motor
GB1415360A (en) * 1973-06-08 1975-11-26 Energy Secretary Of State Explosively operated rapid release valves
US4028886A (en) * 1975-10-23 1977-06-14 Mcdonnell Douglas Corporation Passive chamber wall fragmenter

Also Published As

Publication number Publication date
DE3002977C2 (en) 1982-11-11
GB2068090A (en) 1981-08-05
FR2474593A1 (en) 1981-07-31
FR2474593B1 (en) 1984-04-20
DE3002977A1 (en) 1981-07-30

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee