BE694091A - - Google Patents

Info

Publication number
BE694091A
BE694091A BE694091DA BE694091A BE 694091 A BE694091 A BE 694091A BE 694091D A BE694091D A BE 694091DA BE 694091 A BE694091 A BE 694091A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE694091A publication Critical patent/BE694091A/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/52—Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis
BE694091D 1966-05-19 1967-02-15 BE694091A (zh)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US551397A US3416754A (en) 1966-05-19 1966-05-19 Vectorable exhaust nozzle

Publications (1)

Publication Number Publication Date
BE694091A true BE694091A (zh) 1967-08-16

Family

ID=24201108

Family Applications (1)

Application Number Title Priority Date Filing Date
BE694091D BE694091A (zh) 1966-05-19 1967-02-15

Country Status (5)

Country Link
US (1) US3416754A (zh)
BE (1) BE694091A (zh)
CH (1) CH466721A (zh)
DE (1) DE1481568A1 (zh)
GB (1) GB1161949A (zh)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1277679B (de) * 1967-04-28 1968-09-12 Entwicklungsring Sued G M B H Strahltriebwerk, insbesondere fuer senkrecht startende und landende Flugzeuge, mit schwenkbarer Primaerduese und Zusatzluft ansaugender Sekundaerduese
DE1756879A1 (de) * 1968-07-26 1970-10-01 Karl Jaeger Flugscheibe
US4506848A (en) * 1980-12-22 1985-03-26 British Aerospace Public Limited Company Aircraft configuration and control arrangement therefor
US4478377A (en) * 1980-12-22 1984-10-23 British Aerospace Public Limited Company Aircraft
US4579299A (en) * 1982-04-22 1986-04-01 Morton Thiokol, Inc. Quick turn, 90 degree omniaxial nozzle thrust control system
US4840329A (en) * 1986-04-08 1989-06-20 Rolls-Royce Inc. Aircraft with stowable vectorable nozzle and ejector thrust augmentation
GB2188887B (en) * 1986-04-08 1989-11-29 Rolls Royce Plc Aircraft with stowable vectorable nozzle and ejector thrust augmentation
US4713935A (en) * 1986-04-08 1987-12-22 Rolls-Royce Inc. Vectorable nozzles for aircraft
GB8812978D0 (en) * 1988-06-01 1988-11-16 British Aerospace Nozzle assembly for aircraft
US4901947A (en) * 1989-02-27 1990-02-20 Lockheed Corporation Reverse engine VSTOL
US5351888A (en) * 1993-05-14 1994-10-04 General Electric Company Multi-axis vectorable exhaust nozzle

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025667A (en) * 1957-07-22 1962-03-20 Boeing Co Rotary turret reversible thrust noise suppression jet engine nozzles
DE1066428B (zh) * 1959-01-17
GB915400A (en) * 1960-02-03 1963-01-09 Bristol Siddeley Engines Ltd Improvements in or relating to jet propulsion power plants for aircraft
GB1019303A (en) * 1961-07-31 1966-02-02 Bristol Siddeley Engines Ltd Improvements in nozzle systems of jet propulsion engines
FR1304094A (fr) * 1961-08-04 1962-09-21 Snecma Moteur à réaction convertible de propulsion et de sustentation
GB976854A (en) * 1961-12-07 1964-12-02 Havilland Engine Co Ltd Aircraft propulsion apparatus
GB991220A (en) * 1963-04-25 1965-05-05 Rolls Royce Aircraft

Also Published As

Publication number Publication date
CH466721A (de) 1968-12-15
DE1481568A1 (de) 1969-05-29
GB1161949A (en) 1969-08-20
US3416754A (en) 1968-12-17

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