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ES2034708T3 - Inversor de empuje de turborreactor, con puertas giratorias equilibradas. - Google Patents

Inversor de empuje de turborreactor, con puertas giratorias equilibradas.

Info

Publication number
ES2034708T3
ES2034708T3 ES198989402876T ES89402876T ES2034708T3 ES 2034708 T3 ES2034708 T3 ES 2034708T3 ES 198989402876 T ES198989402876 T ES 198989402876T ES 89402876 T ES89402876 T ES 89402876T ES 2034708 T3 ES2034708 T3 ES 2034708T3
Authority
ES
Spain
Prior art keywords
door panel
turbo
door
pivotally attached
rotating doors
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
ES198989402876T
Other languages
English (en)
Inventor
Claude Achille Germain Dubois
Xavier Raymond Yves Lore
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 ES2034708T3 publication Critical patent/ES2034708T3/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)
  • Ladders (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Wing Frames And Configurations (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
  • Support Devices For Sliding Doors (AREA)

Abstract

LAS PUERTAS (7) PIVOTANTES DE UN INVERSOR DE EMPUJE DEL FLUJO SECUNDARIO DE UN TURBORREACTOR DE DOBLE FLUJO CONSTAN DE UN ELEMENTO INTERNO (11) ASOCIADO A UNA ESTRUCTURA INTERNA (12) Y DE UN ELEMENTO EXTERNO (9), MOVILES EN RELACION MUTUA Y ENLAZADOS POR UNA BIELA (24). EL ELEMENTO INTERNO (11), BAJO LA ACCION DE UN GATO (7A) DE MANIOBRA CUYO VASTAGO (20) ES SOLIDARIO DE UNA ARTICULACION (21) QUE LLEVA DIRECTAMENTE EL ELEMENTO INTERNO (11), PIVOTA ALREDEDOR DE UN PIVOTE PRINCIPAL FIJO (28) QUE LLEVA LA ESTRUCTURA FIJA DEL INVERSOR MIENTRAS QUE EL ELEMENTO EXTERNO (9) PIVOTA ALREDEDOR DE UN PIVOTE SECUNDARIO (31) QUE LLEVA EL ELEMENTO INTERNO (11).
ES198989402876T 1988-10-20 1989-10-18 Inversor de empuje de turborreactor, con puertas giratorias equilibradas. Expired - Lifetime ES2034708T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8813766A FR2638207B1 (fr) 1988-10-20 1988-10-20 Inverseur de poussee de turboreacteur, a portes pivotantes equilibrees

Publications (1)

Publication Number Publication Date
ES2034708T3 true ES2034708T3 (es) 1993-04-01

Family

ID=9371170

Family Applications (1)

Application Number Title Priority Date Filing Date
ES198989402876T Expired - Lifetime ES2034708T3 (es) 1988-10-20 1989-10-18 Inversor de empuje de turborreactor, con puertas giratorias equilibradas.

Country Status (8)

Country Link
US (1) US4960243A (es)
EP (1) EP0365425B1 (es)
AT (1) ATE80205T1 (es)
CA (1) CA1329487C (es)
DE (1) DE68902724T2 (es)
ES (1) ES2034708T3 (es)
FR (1) FR2638207B1 (es)
GR (1) GR3005828T3 (es)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5039171A (en) * 1989-08-18 1991-08-13 Societe Anonyme Dite Hispano-Suiza Multi-panel thrust reverser door
US5120004A (en) * 1990-02-05 1992-06-09 Rohr, Inc. Split door thrust reverser for fan jet aircraft engines
US5243817A (en) * 1990-07-05 1993-09-14 Rohr, Inc. Thrust reverser for fan jet aircraft engines
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.
FR2679605A1 (fr) * 1991-07-24 1993-01-29 Snecma Inverseur de poussee de turboreacteur muni d'un dispositif de securite integre au systeme de commande hydraulique.
FR2683859B1 (fr) * 1991-11-15 1994-02-18 Hispano Suiza Inverseur de poussee de turboreacteur a double flux.
FR2706536B1 (fr) * 1993-06-16 1995-07-21 Snecma Vérin d'inverseur de poussée comportant un dispositif de verrouillage interne et un dispositif de détection de la panne du dispositif de verrouillage interne.
FR2711733B1 (fr) * 1993-10-22 1996-01-26 Hurel Dubois Avions Inverseur de poussée à portes pour moteur d'avion à réaction équipées d'un volet auxiliaire.
US5720449A (en) * 1993-11-19 1998-02-24 Societe De Construction Des Avions Hurel-Dubois Thrust reverser with doors for aircraft engine, equipped with safety systems preventing the untimely opening of the doors
FR2712929B1 (fr) * 1993-11-24 1995-12-29 Hispano Suiza Sa Inverseur de poussée de turboréacteur à double flux.
FR2722534B1 (fr) * 1994-07-13 1996-08-14 Hispano Suiza Sa Inverseur de poussee de turboreacteur double flux, a obstacles externes
FR2730764B1 (fr) * 1995-02-21 1997-03-14 Hispano Suiza Sa Inverseur de poussee a portes associees a un panneau aval
FR2738597B1 (fr) * 1995-09-13 1997-10-03 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes associees a un panneau primaire
FR2740834B1 (fr) 1995-11-02 1997-12-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux muni de portes secondaires
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
FR2764643B1 (fr) * 1997-06-12 1999-07-16 Hispano Suiza Sa Inverseur de poussee a portes de turboreacteur a section variable d'ejection
FR2769953B1 (fr) * 1997-10-16 1999-12-10 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes associees a un panneau amont balance a retenue laterale
US6725541B1 (en) * 2000-01-21 2004-04-27 Rolls-Royce Plc Flow directing element and a method of manufacturing a flow directing element
FR2804474B1 (fr) * 2000-01-27 2002-06-28 Hispano Suiza Sa Inverseur de poussee a grilles aubagees de deviation a structure arriere fixe
US20040149861A1 (en) * 2001-06-06 2004-08-05 Strobl William Charles S & H Cycle Engine
US6845946B2 (en) * 2003-02-21 2005-01-25 The Nordam Group, Inc. Self stowing thrust reverser
GB0606982D0 (en) * 2006-04-07 2006-05-17 Rolls Royce Plc Aeroengine thrust reverser
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
US7735778B2 (en) 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US8051639B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US8172175B2 (en) 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8002217B2 (en) * 2007-11-16 2011-08-23 Spirit Aerosystems, Inc. System for adjustment of thrust reverser pivot door
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
FR2936222B1 (fr) * 2008-09-24 2011-04-01 Aircelle Sa Nacelle a section de tuyere variable
FR2944509B1 (fr) * 2009-04-16 2012-10-19 Aircelle Sa Systeme d'actionnement pour nacelle de turboreacteur
US9617009B2 (en) 2013-02-22 2017-04-11 United Technologies Corporation ATR full ring sliding nacelle
US9822734B2 (en) 2013-02-22 2017-11-21 United Technologies Corporation Tandem thrust reverser with multi-bar linkage
US9435293B2 (en) 2013-02-22 2016-09-06 United Technologies Corporation Full ring sliding nacelle with thrust reverser

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE562528A (es) * 1956-11-21
GB933612A (en) * 1961-02-13 1963-08-08 Rolls Royce Jet engine thrust reversers
GB1181746A (en) * 1968-06-19 1970-02-18 Rolls Royce Thrust Reverser for Jet Propulsion Plant
DE1964976C3 (de) * 1969-12-24 1973-01-04 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Schubumkehrvorrichtung für ein Turbinenstrahltriebwerk eines Flugzeuges
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
US3690561A (en) * 1970-11-05 1972-09-12 Rohr Corp Thrust controlling system
US3764096A (en) * 1972-02-24 1973-10-09 Rohr Industries Inc Thrust reversing apparatus
US3739582A (en) * 1972-04-13 1973-06-19 Rohr Industries Inc Thrust reversing apparatus
DE2241817C3 (de) * 1972-08-25 1975-04-03 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Schubumkehrvorrichtung für ein mit einer Nachverbrennungsanlage ausgerüstetes Turbinenstrahltriebwerk eines Flugzeugs
US4067094A (en) * 1976-04-26 1978-01-10 Harry Feick Co., Inc. Load bearing vane structure for thrust reversal
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
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

Also Published As

Publication number Publication date
EP0365425B1 (fr) 1992-09-02
DE68902724D1 (de) 1992-10-08
FR2638207A1 (fr) 1990-04-27
CA1329487C (fr) 1994-05-17
DE68902724T2 (de) 1993-03-18
US4960243A (en) 1990-10-02
FR2638207B1 (fr) 1990-11-30
GR3005828T3 (es) 1993-06-07
ATE80205T1 (de) 1992-09-15
EP0365425A1 (fr) 1990-04-25

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