ES2041160T3 - Inversor con rejillas sin capo deslizante para turbo-reactor. - Google Patents

Inversor con rejillas sin capo deslizante para turbo-reactor.

Info

Publication number
ES2041160T3
ES2041160T3 ES199090402331T ES90402331T ES2041160T3 ES 2041160 T3 ES2041160 T3 ES 2041160T3 ES 199090402331 T ES199090402331 T ES 199090402331T ES 90402331 T ES90402331 T ES 90402331T ES 2041160 T3 ES2041160 T3 ES 2041160T3
Authority
ES
Spain
Prior art keywords
external door
turbo
internal wing
inverter
reactor
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 - Lifetime
Application number
ES199090402331T
Other languages
English (en)
Inventor
Claude Achille Germain Dubois
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.)
Safran Transmission Systems SAS
Original Assignee
Hispano Suiza SA
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 Hispano Suiza SA filed Critical Hispano Suiza SA
Application granted granted Critical
Publication of ES2041160T3 publication Critical patent/ES2041160T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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)
  • Transmission Devices (AREA)
  • Magnetic Resonance Imaging Apparatus (AREA)

Abstract

UN INVERSOR DE EMPUJE PARA TURBO-REACTOR CONSTA DE UNAS PUERTAS PIVOTANTES QUE CONSTAN, CADA UNA DE ELLAS, DE UNA PUERTA EXTERNA (9) Y UN ALERON INTERNO (11) QUE CONSTITUYE EL OBSTACULO DE DESVIACION DEL FLUJO (27) EN POSICION DESPLEGADA. LA MANIOBRA DE LA PUERTA SE OBTIENE MEDIANTE UN TORNILLO DE BOLAS (21) CUYA TUERCA (22) ESTA ENLAZADA RESPECTIVAMENTE A LA PUERTA EXTERNA (9) Y AL ALERON INTERNO (11) MEDIANTE BIELITAS (23,24), PIVOTANDO LA PUERTA EXTERNA (9) ALREDEDOR DE UN PIVOTE PRINCIPAL FIJO (19) Y EL ALERON INTERNO (11) PIVOTA ALREDEDOR DE UN PIVOTE SECUNDARIO (20) QUE LO ARRASTRA IGUALMENTE EN DESLIZAMIENTO HACIA ATRAS. A AMBOS LADOS DE DICHO TORNILLO DE BOLAS (21) HAY UNAS REJILLAS DE EXPULSION (25) QUE PERMITEN EL CONTROL EN DIRECCION DEL FLUJO INVERTIDO (27) Y DISPUESTAS EN LA POSICION DE EMPUJE DIRECTO ENTRE LA PUERTA EXTERNA (9) Y EL ALERON INTERNO (11).
ES199090402331T 1989-08-23 1990-08-22 Inversor con rejillas sin capo deslizante para turbo-reactor. Expired - Lifetime ES2041160T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8911155A FR2651278B1 (fr) 1989-08-23 1989-08-23 Inverseur a grilles sans capot coulissant pour turboreacteur.

Publications (1)

Publication Number Publication Date
ES2041160T3 true ES2041160T3 (es) 1993-11-01

Family

ID=9384867

Family Applications (1)

Application Number Title Priority Date Filing Date
ES199090402331T Expired - Lifetime ES2041160T3 (es) 1989-08-23 1990-08-22 Inversor con rejillas sin capo deslizante para turbo-reactor.

Country Status (6)

Country Link
US (1) US5090197A (es)
EP (1) EP0414609B1 (es)
CA (1) CA2022448C (es)
DE (1) DE69001731T2 (es)
ES (1) ES2041160T3 (es)
FR (1) FR2651278B1 (es)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2683859B1 (fr) * 1991-11-15 1994-02-18 Hispano Suiza Inverseur de poussee de turboreacteur a double flux.
US5255850A (en) * 1992-06-29 1993-10-26 The United States Of America As Represented By The Secretary Of The Air Force Pivoting flaps and vane pack in a nozzle reverser assembly
FR2698913B1 (fr) * 1992-12-04 1995-02-03 Hurel Dubois Avions Ensemble d'inversion de poussée à portes équipé d'un dispositif de contrôle de jet.
US5315821A (en) * 1993-02-05 1994-05-31 General Electric Company Aircraft bypass turbofan engine thrust reverser
FR2730763B1 (fr) * 1995-02-21 1997-03-14 Hispano Suiza Sa Inverseur de poussee a volets aval pour turboreacteur
FR2738291B1 (fr) * 1995-09-06 1997-09-26 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes associees a un panneau amont formant ecope
FR2741910B1 (fr) * 1995-11-30 1998-01-02 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes a panneau arriere articule
FR2751377B1 (fr) * 1996-07-18 1998-09-04 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes comportant un panneau coulissant
FR2757215B1 (fr) * 1996-12-12 1999-01-22 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes comportant des aubes deflectrices associees a la structure fixe
FR2757901B1 (fr) * 1996-12-26 1999-01-29 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux a coquilles aval
US20040149861A1 (en) * 2001-06-06 2004-08-05 Strobl William Charles S & H Cycle Engine
FR2849113B1 (fr) * 2002-12-24 2005-02-04 Hurel Hispano Inverseur de poussee a grilles de deflection optimisees
US6845946B2 (en) * 2003-02-21 2005-01-25 The Nordam Group, Inc. Self stowing thrust reverser
US20110101158A1 (en) * 2005-03-29 2011-05-05 The Boeing Company Thrust Reversers Including Monolithic Components
US7690190B2 (en) * 2005-05-11 2010-04-06 The Boeing Company Aircraft systems including cascade thrust reversers
US7559507B2 (en) * 2005-06-27 2009-07-14 The Boeing Company Thrust reversers including locking assemblies for inhibiting deflection
US7600371B2 (en) 2005-10-18 2009-10-13 The Boeing Company Thrust reversers including support members for inhibiting deflection
US8015797B2 (en) * 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
US20080134664A1 (en) * 2006-12-06 2008-06-12 Spirit Aerosystems, Inc. Thrust reverser pin lock
EP2479414B1 (en) 2007-08-08 2015-06-10 Rohr, Inc. Variable area fan nozzle with bypass flow
US9759087B2 (en) 2007-08-08 2017-09-12 Rohr, Inc. Translating variable area fan nozzle providing an upstream bypass flow exit
FR2921976B1 (fr) * 2007-10-08 2009-12-04 Aircelle Sa Actionneur pour structure mobile de nacelle d'aeronef, et nacelle comprenant au moins un tel actionneur
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8172175B2 (en) 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8051639B2 (en) * 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US7735778B2 (en) 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
FR2944509B1 (fr) * 2009-04-16 2012-10-19 Aircelle Sa Systeme d'actionnement pour nacelle de turboreacteur
DE102011008918A1 (de) * 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinenschubumkehrvorrichtung
US9181898B2 (en) * 2011-09-20 2015-11-10 United Technologies Corporation Thrust reverser for a gas turbine engine with moveable doors
GB201219368D0 (en) 2012-10-29 2012-12-12 Rolls Royce Deutschland Aeroengine thrust reverser arrangement
US9631578B2 (en) 2013-02-22 2017-04-25 United Technologies Corporation Pivot thrust reverser surrounding inner surface of bypass duct
US9617009B2 (en) 2013-02-22 2017-04-11 United Technologies Corporation ATR full ring sliding nacelle
FR3006716B1 (fr) * 2013-06-10 2015-06-05 Aircelle Sa Inverseur de poussee a volet de blocage articule par embiellage trois points
US10724475B2 (en) * 2016-09-27 2020-07-28 The Boeing Company Dual turn thrust reverser cascade systems and methods
US10415503B2 (en) 2017-03-10 2019-09-17 Spirit Aerosystems, Inc. Cascade pivot door-type thrust reverser for turbofan engine
FR3074855A1 (fr) * 2017-12-11 2019-06-14 Airbus Operations Grille pour la formation d'un flux d'inversion d'un turboreacteur d'aeronef
FR3076323B1 (fr) * 2017-12-28 2020-01-10 Safran Nacelles Inverseur de poussee a grilles pour turboreacteur
US12270356B2 (en) * 2022-08-01 2025-04-08 Rohr, Inc. Thrust reverser cascade with one or more flow disrupters

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
US3511055A (en) * 1968-05-29 1970-05-12 Rohr Corp Thrust reverser
GB1181746A (en) * 1968-06-19 1970-02-18 Rolls Royce Thrust Reverser for Jet Propulsion Plant
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
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
FR2486153B1 (fr) * 1980-07-04 1985-10-04 Hurel Dubois Avions Inverseur de poussee pour moteur a reaction, destine notamment a equiper un aeronef
FR2506843B1 (fr) * 1981-05-29 1987-04-24 Hurel Dubois Avions Dispositif d'inversion de poussee pour turboreacteur d'avion
FR2559838B1 (fr) * 1984-02-21 1988-05-13 Hurel Dubois Avions Procede et dispositif permettant le controle du jet inverse dans les moteurs a reaction a inverseur de poussee
FR2618853B1 (fr) * 1987-07-29 1989-11-10 Hispano Suiza Sa Inverseur de poussee de turboreacteur muni d'un deflecteur mobile de porte
FR2622929A1 (fr) * 1987-11-05 1989-05-12 Hispano Suiza Sa Inverseur de poussee de turboreacteur a grilles,a section variable d'ejection

Also Published As

Publication number Publication date
EP0414609B1 (fr) 1993-05-26
CA2022448A1 (fr) 1991-02-24
FR2651278B1 (fr) 1994-05-06
FR2651278A1 (fr) 1991-03-01
CA2022448C (fr) 2000-10-03
DE69001731D1 (de) 1993-07-01
DE69001731T2 (de) 1993-10-14
EP0414609A1 (fr) 1991-02-27
US5090197A (en) 1992-02-25

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