BE682001A - - Google Patents

Info

Publication number
BE682001A
BE682001A BE682001DA BE682001A BE 682001 A BE682001 A BE 682001A BE 682001D A BE682001D A BE 682001DA BE 682001 A BE682001 A BE 682001A
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 BE682001A publication Critical patent/BE682001A/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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE682001D 1965-06-07 1966-06-02 BE682001A (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US462789A US3280561A (en) 1965-06-07 1965-06-07 Thrust reverser mechanism

Publications (1)

Publication Number Publication Date
BE682001A true BE682001A (en:Method) 1966-11-14

Family

ID=23837759

Family Applications (1)

Application Number Title Priority Date Filing Date
BE682001D BE682001A (en:Method) 1965-06-07 1966-06-02

Country Status (3)

Country Link
US (1) US3280561A (en:Method)
BE (1) BE682001A (en:Method)
DE (1) DE1279478B (en:Method)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3056721A1 (en) * 2015-02-13 2016-08-17 United Technologies Corporation Turbine engine with a turbo-compressor

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1111219A (en) * 1966-02-14 1968-04-24 Rolls Royce Gas turbine engine
US3465524A (en) * 1966-03-02 1969-09-09 Rolls Royce Fan gas turbine engine
GB1085619A (en) * 1966-03-09 1967-10-04 Rolls Royce Gas turbine engine
US3476486A (en) * 1966-04-12 1969-11-04 Dowty Rotol Ltd Gas turbine engines
US3366349A (en) * 1966-05-02 1968-01-30 Gen Dynamics Corp Centerbody thrust reverser
US3330115A (en) * 1966-05-31 1967-07-11 United Aircraft Corp Turbofan thrust reverser
US3353355A (en) * 1966-05-31 1967-11-21 United Aircraft Corp Turbofan lightweight thrust reverser
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
US3531049A (en) * 1968-09-09 1970-09-29 Rohr Corp Unitary ejector-thrust reverser assembly for jet-propulsion engines
US3570767A (en) * 1969-10-01 1971-03-16 Rohr Corp Thrust reversing apparatus
US3874620A (en) * 1973-03-09 1975-04-01 Boeing Co Reversing apparatus for a jet engine
US3981463A (en) * 1974-03-21 1976-09-21 Rohr Industries, Inc. Overwing thrust reverser
US3917198A (en) * 1974-06-21 1975-11-04 Rohr Industries Inc Overwing post exit blocker/deflector door thrust reverser
US4278220A (en) * 1979-03-30 1981-07-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thrust reverser for a long duct fan engine
FR2550821B1 (fr) * 1983-08-18 1985-11-08 Snecma Dispositif variateur du flux secondaire d'un turboreacteur multiflux
FR2618852B1 (fr) * 1987-07-29 1989-11-10 Hispano Suiza Sa Inverseur de poussee de turboreacteur muni d'un dispositif redresseur de flux
FR2625261B1 (fr) * 1987-12-23 1992-11-06 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles lies au capot primaire
FR2650861A1 (fr) * 1989-08-08 1991-02-15 Snecma Inverseur de poussee de turboreacteur double flux, a obstacles lies au capot primaire
FR2676780B1 (fr) * 1991-05-23 1993-08-13 Snecma Inverseur de poussee pour turbosoufflante a tres grand taux dilution.
FR2678026B1 (fr) * 1991-06-24 1993-10-15 Hurel Dubois Avions Perfectionnement aux inverseurs de poussee de moteur a reaction.
FR2721977B1 (fr) 1994-06-30 1996-08-02 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux a obstacles lies au capot primaire
FR2749041B1 (fr) * 1996-05-23 1998-06-26 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux a obstacles lies au capot primaire
FR2759418B1 (fr) * 1997-02-13 1999-03-19 Snecma Inverseur de poussee pour turbosoufflante a tres grand taux de dilution
US8720182B2 (en) * 2006-10-12 2014-05-13 United Technologies Corporation Integrated variable area nozzle and thrust reversing mechanism
FR2916484B1 (fr) * 2007-05-21 2009-07-24 Aircelle Sa Porte a becquet mobile pour inverseur de poussee a porte
US9650992B2 (en) * 2013-10-17 2017-05-16 Rohr, Inc. Core cowl thrust reverser system and apparatus
US10041408B2 (en) 2015-02-13 2018-08-07 United Technologies Corporation Turbine engine with a turbo-compressor
US10337401B2 (en) 2015-02-13 2019-07-02 United Technologies Corporation Turbine engine with a turbo-compressor
US10100731B2 (en) 2015-02-13 2018-10-16 United Technologies Corporation Turbine engine with a turbo-compressor
US10077740B2 (en) 2015-10-16 2018-09-18 The Boeing Company Folding door thrust reversers for aircraft engines

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE23198E (en) * 1950-02-21 Reaction propelling device for
US2396911A (en) * 1939-12-04 1946-03-19 Anxionnaz Rene Reaction propelling device for aircraft
US2945346A (en) * 1954-10-04 1960-07-19 Republic Aviat Corp Reverse thrust brake
US2929580A (en) * 1956-06-18 1960-03-22 Piasecki Aircraft Corp Aircraft for vertical or short takeoff, and integrated propulsion lifting and propeller slip stream deflecting unit therefor
FR1286886A (fr) * 1961-01-27 1962-03-09 Nord Aviation Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux
US3040524A (en) * 1961-07-28 1962-06-26 United Aircraft Corp Ducted fan engine thrust reverser

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3056721A1 (en) * 2015-02-13 2016-08-17 United Technologies Corporation Turbine engine with a turbo-compressor

Also Published As

Publication number Publication date
US3280561A (en) 1966-10-25
DE1279478B (de) 1968-10-03

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