BE682002A - - Google Patents

Info

Publication number
BE682002A
BE682002A BE682002DA BE682002A BE 682002 A BE682002 A BE 682002A BE 682002D A BE682002D A BE 682002DA BE 682002 A BE682002 A BE 682002A
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 BE682002A publication Critical patent/BE682002A/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
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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)
BE682002D 1965-06-07 1966-06-02 BE682002A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US462790A US3262268A (en) 1965-06-07 1965-06-07 Thrust reverser

Publications (1)

Publication Number Publication Date
BE682002A true BE682002A (fr) 1966-11-14

Family

ID=23837762

Family Applications (1)

Application Number Title Priority Date Filing Date
BE682002D BE682002A (fr) 1965-06-07 1966-06-02

Country Status (4)

Country Link
US (1) US3262268A (fr)
BE (1) BE682002A (fr)
DE (1) DE1456037B1 (fr)
GB (1) GB1085780A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2960029A1 (fr) * 2010-05-17 2011-11-18 Aircelle Sa Inverseur de poussee a grilles ou a cascade, pour un turboreacteur d’avion
WO2014207410A1 (fr) * 2013-06-27 2014-12-31 Aircelle Inverseur à doubles grilles sans bielles dans la veine

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
GB1150012A (en) * 1966-09-12 1969-04-30 Rolls Royce Fluid Flow Duct Including Thrust Reversing Means
US3503211A (en) * 1968-04-10 1970-03-31 Rohr Corp Thrust reverser
US3500644A (en) * 1968-04-10 1970-03-17 Rohr Corp Thrust reverser
GB1247691A (en) * 1968-08-08 1971-09-29 Rolls Royce Improvements in or relating to fan ducts for gas turbine ducted fan engines
US3541794A (en) * 1969-04-23 1970-11-24 Gen Electric Bifurcated fan duct thrust reverser
US3600894A (en) * 1970-04-28 1971-08-24 Rohr Corp Thrust reversing apparatus
US3717304A (en) * 1970-05-06 1973-02-20 Rolls Royce Thrust reverser for fluid flow engine
US3665709A (en) * 1970-06-04 1972-05-30 Rohr Corp Thrust reversing apparatus
US3658253A (en) * 1970-07-01 1972-04-25 Fred W Steffen Thrust reverser for plug type jet engine nozzle
US3814324A (en) * 1972-06-19 1974-06-04 Gen Electric Propulsion nozzle and actuator system employed therein
US3837577A (en) * 1973-06-29 1974-09-24 United Aircraft Corp Minimum drag variable area exhaust nozzle
US3920203A (en) * 1974-12-23 1975-11-18 Boeing Co Thrust control apparatus for obtaining maximum thrust reversal in minimum time upon landing of an aircraft
US4067094A (en) * 1976-04-26 1978-01-10 Harry Feick Co., Inc. Load bearing vane structure for thrust reversal
US4205813A (en) * 1978-06-19 1980-06-03 General Electric Company Thrust vectoring apparatus for a VTOL aircraft
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
US4533098A (en) * 1983-06-20 1985-08-06 General Electric Company Thrust reverser attachment
FR2621082A1 (fr) * 1987-09-30 1989-03-31 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes munies d'une plaque au profil de veine
FR2627807B1 (fr) * 1988-02-25 1990-06-29 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux equipe de bords de deviation munis de levres mobiles
US4922712A (en) * 1988-03-28 1990-05-08 General Electric Company Thrust reverser for high bypass turbofan engine
US5046307A (en) * 1988-03-28 1991-09-10 General Electric Company Thrust reverser for high bypass turbofan engine
US5228641A (en) * 1991-08-15 1993-07-20 Rohr, Inc. Cascade type aircraft engine thrust reverser with hidden link actuator
US5309711A (en) * 1991-08-21 1994-05-10 Rohr, Inc. Cascade type thrust reverser for fan jet engines
GB0608985D0 (en) * 2006-05-06 2006-06-14 Rolls Royce Plc Aeroengine thrust reverser
EP2074306A1 (fr) 2006-10-12 2009-07-01 United Technologies Corporation Buse d'éjection à section variable intégrée à double cascade de fonctions et inverseur de poussée
FR2907512B1 (fr) * 2006-10-23 2008-12-12 Aircelle Sa Inverseur de poussee a grilles pour moteur a reaction
US8006479B2 (en) 2007-10-15 2011-08-30 United Technologies Corporation Thrust reversing variable area nozzle
FR2946094B1 (fr) * 2009-06-02 2014-04-18 Aircelle Sa Inverseur de poussee pour nacelle de turboreacteur double flux.
FR2960918B1 (fr) * 2010-06-08 2012-05-25 Aircelle Sa Grille de deviation du type autosupporte pour inverseur de poussee
FR2966883B1 (fr) * 2010-11-03 2012-11-02 Aircelle Sa Dispositif d'inversion de poussee sans bielle dans la veine
GB201219366D0 (en) * 2012-10-29 2012-12-12 Rolls Royce Deutschland & Co Kg Aeroengine thrust reverser arrangement
US10006405B2 (en) * 2012-11-30 2018-06-26 General Electric Company Thrust reverser system with translating-rotating blocker doors and method of operation
US10077739B2 (en) * 2014-04-24 2018-09-18 Rohr, Inc. Dual actuation system for cascade and thrust reverser panel for an integral cascade variable area fan nozzle
US10309343B2 (en) * 2014-11-06 2019-06-04 Rohr, Inc. Split sleeve hidden door thrust reverser
DE102015203219A1 (de) * 2015-02-23 2016-08-25 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung einer Gasturbine mit Schubumkehrvorrichtung und im Querschnitt verstellbarer Ausströmdüse
US10378480B2 (en) * 2017-02-10 2019-08-13 Rohr, Inc Blocker door stiffening features
FR3102511B1 (fr) * 2019-10-25 2022-08-26 Safran Nacelles Inverseur de poussée à volets commandés par un mécanisme doté de guignols aéronautiques
EP3943737A1 (fr) * 2020-04-07 2022-01-26 Rohr, Inc. Système inverseur de poussée à volet caché pour système de propulsion d'aéronef

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE860754C (de) * 1944-07-04 1952-12-22 Daimler Benz Ag Gasstroemungsmaschine, insbesondere Strahltriebwerk fuer Luftfahrzeuge od. dgl.
BE524592A (fr) * 1952-11-25
US2950595A (en) * 1954-11-01 1960-08-30 Marquardt Corp Thrust reverser
US2847823A (en) * 1955-03-15 1958-08-19 Curtiss Wright Corp Reverse thrust nozzle construction
US3113428A (en) * 1957-03-13 1963-12-10 Rolls Royce Silenced jet propulsion nozzle with thrust reversing means
FR1286886A (fr) * 1961-01-27 1962-03-09 Nord Aviation Dispositif d'inversion de poussée pour propulseurs comportant un turbo-réacteur àdouble flux
NL247267A (fr) * 1958-04-02
US2938335A (en) * 1958-04-14 1960-05-31 Boeing Co Noise suppressor and thrust reverser
US3068646A (en) * 1959-01-28 1962-12-18 Rolls Royce Improvements in by-pass type gas turbine engines
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines
DE1187491B (de) * 1960-03-07 1965-02-18 Moteuers D Aviat Soc Nat D Etu Stroemungskanal mit ringfoermigem Querschnitt und seitlichen Strahlumlenkungsoeffnungen

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2960029A1 (fr) * 2010-05-17 2011-11-18 Aircelle Sa Inverseur de poussee a grilles ou a cascade, pour un turboreacteur d’avion
WO2011144837A1 (fr) * 2010-05-17 2011-11-24 Aircelle Inverseur de poussée à grilles ou à cascade, pour un turboréacteur d'avion
US9109540B2 (en) 2010-05-17 2015-08-18 Aircelle Airplane jet engine thrust reverser having gratings or cascades
WO2014207410A1 (fr) * 2013-06-27 2014-12-31 Aircelle Inverseur à doubles grilles sans bielles dans la veine
FR3007799A1 (fr) * 2013-06-27 2015-01-02 Aircelle Sa Inverseur a doubles grilles sans bielles dans la veine

Also Published As

Publication number Publication date
DE1456037B1 (de) 1970-10-01
GB1085780A (en) 1967-10-04
US3262268A (en) 1966-07-26

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