FR1303929A - Perfectionnements aux moteurs de propulsion par réaction - Google Patents

Perfectionnements aux moteurs de propulsion par réaction

Info

Publication number
FR1303929A
FR1303929A FR876280A FR876280A FR1303929A FR 1303929 A FR1303929 A FR 1303929A FR 876280 A FR876280 A FR 876280A FR 876280 A FR876280 A FR 876280A FR 1303929 A FR1303929 A FR 1303929A
Authority
FR
France
Prior art keywords
jet propulsion
propulsion engines
engines
jet
propulsion
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
FR876280A
Other languages
English (en)
French (fr)
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.)
Bristol Siddeley Engines Ltd
Original Assignee
Bristol Siddeley Engines Ltd
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 Bristol Siddeley Engines Ltd filed Critical Bristol Siddeley Engines Ltd
Application granted granted Critical
Publication of FR1303929A publication Critical patent/FR1303929A/fr
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
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002Plants 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
    • F02K1/004Plants 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/38Jet flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
FR876280A 1960-10-21 1961-10-18 Perfectionnements aux moteurs de propulsion par réaction Expired FR1303929A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB36261/60A GB953803A (en) 1960-10-21 1960-10-21 Improvements in or relating to jet propulsion engines

Publications (1)

Publication Number Publication Date
FR1303929A true FR1303929A (fr) 1962-09-14

Family

ID=10386493

Family Applications (1)

Application Number Title Priority Date Filing Date
FR876280A Expired FR1303929A (fr) 1960-10-21 1961-10-18 Perfectionnements aux moteurs de propulsion par réaction

Country Status (4)

Country Link
US (1) US3180087A (sv)
DE (1) DE1210259B (sv)
FR (1) FR1303929A (sv)
GB (1) GB953803A (sv)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5769317A (en) * 1995-05-04 1998-06-23 Allison Engine Company, Inc. Aircraft thrust vectoring system
US5699662A (en) * 1996-05-28 1997-12-23 Lockheed Martin Corporation Infrared suppression exhaust duct system for a turboprop propulsion system for an aircraft
US6382559B1 (en) 1999-08-13 2002-05-07 Rolls-Royce Corporation Thrust vectoring mechanism
ATE523682T1 (de) 2005-09-27 2011-09-15 Volvo Aero Corp Anordnung zum antrieb eines flugzeugs, flugzeug und auslassdüse für ein düsentriebwerk
US9976514B2 (en) * 2015-08-27 2018-05-22 Rolls-Royce North American Technologies, Inc. Propulsive force vectoring
EP3181455B1 (en) 2015-12-16 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sections
WO2019094804A1 (en) * 2017-11-09 2019-05-16 Abe Karem Devices and methods for exhaust vectoring in tilt rotor aircraft

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2631425A (en) * 1948-09-11 1953-03-17 Bofors Ab Compression nozzle for ram-jet engines
GB675300A (en) * 1949-05-24 1952-07-09 Rolls Royce Improvements in or relating to exhaust ducting of gas-turbine engines
GB695482A (en) * 1950-11-28 1953-08-12 Rolls Royce Improvements in or relating to gas-turbine engines
US2699647A (en) * 1951-06-05 1955-01-18 Rohr Aircraft Corp Adjustable nozzle for exhaust gas
GB757981A (en) * 1952-02-06 1956-09-26 Rolls Royce Improvements in or relating to gas turbine engines
US2933891A (en) * 1953-06-23 1960-04-26 Rolls Royce Jet pipe arrangements for jet propulsion engines
GB755019A (en) * 1953-09-09 1956-08-15 Rolls Royce Improvements in or relating to jet-propelled aircraft
CH327871A (de) * 1954-10-26 1958-02-15 Rolls Royce Strahlrohreinrichtung an einem Strahltriebwerk
FR1139775A (fr) * 1954-11-26 1957-07-04 Power Jets Res & Dev Ltd Tuyère de décharge pour un jet propulseur
US2912188A (en) * 1955-09-15 1959-11-10 Bell Aircraft Corp Jet propelled aircraft with tiltable combustion chambers
US2846844A (en) * 1956-01-24 1958-08-12 Ryan Aeronautical Co Variable area thrust deflectoraugmenter for jet engines
US2879014A (en) * 1957-07-02 1959-03-24 Bell Aircraft Corp Jet propelled airplane with jet diverter
US3025667A (en) * 1957-07-22 1962-03-20 Boeing Co Rotary turret reversible thrust noise suppression jet engine nozzles
US2936973A (en) * 1957-09-06 1960-05-17 Gen Electric Vtol aircraft
DE1066428B (sv) * 1959-01-17
US3041830A (en) * 1959-08-17 1962-07-03 Rolls Royce Steering deflector for a turbo-fan engine

Also Published As

Publication number Publication date
DE1210259C2 (sv) 1966-08-11
GB953803A (en) 1964-04-02
DE1210259B (de) 1966-02-03
US3180087A (en) 1965-04-27

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