DE3273006D1 - Thrust reverser for a jet engine - Google Patents

Thrust reverser for a jet engine

Info

Publication number
DE3273006D1
DE3273006D1 DE8282400968T DE3273006T DE3273006D1 DE 3273006 D1 DE3273006 D1 DE 3273006D1 DE 8282400968 T DE8282400968 T DE 8282400968T DE 3273006 T DE3273006 T DE 3273006T DE 3273006 D1 DE3273006 D1 DE 3273006D1
Authority
DE
Germany
Prior art keywords
jet engine
thrust reverser
reverser
thrust
jet
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
DE8282400968T
Other languages
English (en)
Inventor
Alain Fournier
John Kennedy
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.)
Hurel Hispano Meudon SA
Original Assignee
Societe de Construction des Avions Hurel Dubois
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 Societe de Construction des Avions Hurel Dubois filed Critical Societe de Construction des Avions Hurel Dubois
Application granted granted Critical
Publication of DE3273006D1 publication Critical patent/DE3273006D1/de
Expired legal-status Critical Current

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
    • 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)
  • Power-Operated Mechanisms For Wings (AREA)
  • Superstructure Of Vehicle (AREA)
DE8282400968T 1981-05-29 1982-05-26 Thrust reverser for a jet engine Expired DE3273006D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8110693A FR2506843B1 (fr) 1981-05-29 1981-05-29 Dispositif d'inversion de poussee pour turboreacteur d'avion

Publications (1)

Publication Number Publication Date
DE3273006D1 true DE3273006D1 (de) 1986-10-09

Family

ID=9259003

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8282400968T Expired DE3273006D1 (de) 1981-05-29 1982-05-26 Thrust reverser for a jet engine

Country Status (4)

Country Link
US (1) US4485970A (de)
EP (1) EP0067747B1 (de)
DE (1) DE3273006D1 (de)
FR (1) FR2506843B1 (de)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2601077B1 (fr) * 1986-07-07 1988-10-21 Hurel Dubois Avions Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.
FR2611233B1 (fr) * 1987-02-19 1991-05-10 Hurel Dubois Avions Groupe moto-propulseur d'avion du type a ventilateur capote equipe d'un inverseur de poussee a portes
FR2618853B1 (fr) * 1987-07-29 1989-11-10 Hispano Suiza Sa Inverseur de poussee de turboreacteur muni d'un deflecteur mobile de porte
FR2618852B1 (fr) * 1987-07-29 1989-11-10 Hispano Suiza Sa Inverseur de poussee de turboreacteur muni d'un dispositif redresseur de flux
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
FR2622928A1 (fr) * 1987-11-05 1989-05-12 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes,a section variable d'ejection
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
FR2634251B1 (fr) * 1988-07-18 1993-08-13 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux equipe de bords de deviation mobiles
FR2635825B1 (fr) * 1988-08-29 1990-11-30 Hurel Dubois Avions Inverseur de poussee pour moteur a reaction de type a portes equipees de volets auxiliaires
FR2638207B1 (fr) * 1988-10-20 1990-11-30 Hispano Suiza Sa Inverseur de poussee de turboreacteur, a portes pivotantes equilibrees
FR2638784B1 (fr) * 1988-11-09 1990-12-21 Hispano Suiza Sa Inverseur de poussee de turboreacteur muni de portes a mini-tuyere de deviation du flux inverse
US5039171A (en) * 1989-08-18 1991-08-13 Societe Anonyme Dite Hispano-Suiza Multi-panel thrust reverser door
FR2651278B1 (fr) * 1989-08-23 1994-05-06 Hispano Suiza Inverseur a grilles sans capot coulissant pour turboreacteur.
US5230213A (en) * 1991-06-12 1993-07-27 Rohr, Inc. Aircraft turbine engine thrust reverser
FR2678026B1 (fr) * 1991-06-24 1993-10-15 Hurel Dubois Avions Perfectionnement aux inverseurs de poussee de moteur a reaction.
US5197693A (en) * 1991-08-15 1993-03-30 Rohr, Inc. Aircraft turbine engine thrust reverser with sliding hinge actuator
FR2680547B1 (fr) * 1991-08-21 1993-10-15 Hispano Suiza Inverseur de poussee de turboreacteur ayant un bord de deviation a courbure evolutive.
FR2681101B1 (fr) * 1991-09-11 1993-11-26 Hispano Suiza Inverseur de poussee de turboreacteur a pilotage ameliore des nappes du flux inverse.
US5224342A (en) * 1992-02-13 1993-07-06 Lair Jean Pierre Latching and sealing arrangement for jet engine thrust reverser
FR2728626B1 (fr) * 1994-12-21 1998-03-06 Hurel Dubois Avions Inverseur de poussee pour moteur a reaction a bord de deviation amenage
US5615834A (en) * 1995-01-31 1997-04-01 Osman; Medhat A. Ultra thrust reverser system
FR2730764B1 (fr) * 1995-02-21 1997-03-14 Hispano Suiza Sa Inverseur de poussee a portes associees a un panneau aval
FR2730763B1 (fr) * 1995-02-21 1997-03-14 Hispano Suiza Sa Inverseur de poussee a volets aval pour turboreacteur
DE69521806D1 (de) * 1995-09-13 2001-08-23 Hurel Dubois Avions Strahlumkehrgitter für eine Schubumkehrvorrichtungsklappe
FR2742482B1 (fr) * 1995-12-19 1998-02-06 Hurel Dubois Avions Inverseur de poussee a tuyere a section reglable pour moteur d'avion a reaction
DE69616739T2 (de) * 1996-02-08 2002-09-05 Hurel Dubois Avions Dichtungsanordnung für schwenkbare Schubumkehrklappe
FR2754313B1 (fr) * 1996-10-03 1999-01-08 Hispano Suiza Sa Inverseur de poussee a portes a installation de verin de commande optimisee
US5833140A (en) * 1996-12-12 1998-11-10 United Technologies Corporation Variable geometry exhaust nozzle for a turbine engine
EP0852290A1 (de) * 1996-12-19 1998-07-08 SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) Schubumkehrvorrichtung für ein Bläsertriebwerk
EP0926333A1 (de) 1997-12-26 1999-06-30 SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) Konfiguration einer Schubumkehrvorrichtung
EP1215118B1 (de) * 2000-12-18 2005-07-27 Techspace Aero S.A. Prüfstand für Schubumkehr
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
FR2871776B1 (fr) * 2004-06-21 2007-11-02 Snecma Moteurs Sa Procede de freinage d'un avion et turboreacteur a double flux pour la mise en oeuvre du procede
EP2074308B1 (de) * 2006-10-12 2011-12-21 United Technologies Corporation Integrierter mechanismus aus einer düse mit variablem querschnitt und schubumkehrvorrichtung
WO2014092757A1 (en) * 2012-12-11 2014-06-19 United Technologies Corporation Asymmetric thrust reversers
US9435293B2 (en) 2013-02-22 2016-09-06 United Technologies Corporation Full ring sliding nacelle with thrust reverser
US9822734B2 (en) 2013-02-22 2017-11-21 United Technologies Corporation Tandem thrust reverser with multi-bar linkage
US9573695B2 (en) 2013-02-22 2017-02-21 United Technologies Corporation Integrated nozzle and plug
US9845769B2 (en) * 2015-05-05 2017-12-19 Rohr, Inc. Plastic core blocker door
US11300077B2 (en) * 2018-10-02 2022-04-12 Rohr, Inc. Deployable fairing for door reversers systems and methods
US11346304B2 (en) 2018-09-06 2022-05-31 Rohr, Inc. Thrust reverser single degree of freedom actuator mechanism systems and methods
US11333102B2 (en) 2018-09-06 2022-05-17 Rohr, Inc. Thrust reverser actuation arrangement and deployable fairing systems and methods

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE464035A (de) * 1945-03-22 1900-01-01
US3113428A (en) * 1957-03-13 1963-12-10 Rolls Royce Silenced jet propulsion nozzle with thrust reversing means
US3279182A (en) * 1965-06-07 1966-10-18 Gen Electric Thrust reverser
FR1482538A (fr) * 1965-06-07 1967-05-26 Gen Electric Inverseur de poussée
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
GB1177864A (en) * 1968-04-09 1970-01-14 Rolls Royce Thrust Reverser or Spoiler
US3531049A (en) * 1968-09-09 1970-09-29 Rohr Corp Unitary ejector-thrust reverser assembly for jet-propulsion engines
US3647141A (en) * 1970-06-01 1972-03-07 Rohr Corp Thrust controlling apparatus
US3601992A (en) * 1970-06-10 1971-08-31 Rohr Corp Thrust reversing apparatus
US3605411A (en) * 1970-07-01 1971-09-20 Rohr Corp Thrust reversing apparatus
US3699682A (en) * 1971-01-04 1972-10-24 Mc Donnell Douglas Corp Turbofan engine thrust reverser
FR2146109A1 (de) * 1971-07-19 1973-03-02 Bruner Georges
US3764096A (en) * 1972-02-24 1973-10-09 Rohr Industries Inc Thrust reversing apparatus
US4052007A (en) * 1975-11-25 1977-10-04 United Technologies Corporation Flap-type two-dimensional nozzle
FR2486153B1 (fr) * 1980-07-04 1985-10-04 Hurel Dubois Avions Inverseur de poussee pour moteur a reaction, destine notamment a equiper un aeronef

Also Published As

Publication number Publication date
EP0067747A1 (de) 1982-12-22
EP0067747B1 (de) 1986-09-03
US4485970A (en) 1984-12-04
FR2506843B1 (fr) 1987-04-24
FR2506843A1 (fr) 1982-12-03

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: HUREL-HISPANO MEUDON S.A., MEUDON-LA-FORET, FR