GR3018892T3 - Thrust-reverser with improved guidance of the reversed jets. - Google Patents

Thrust-reverser with improved guidance of the reversed jets.

Info

Publication number
GR3018892T3
GR3018892T3 GR960400289T GR960400289T GR3018892T3 GR 3018892 T3 GR3018892 T3 GR 3018892T3 GR 960400289 T GR960400289 T GR 960400289T GR 960400289 T GR960400289 T GR 960400289T GR 3018892 T3 GR3018892 T3 GR 3018892T3
Authority
GR
Greece
Prior art keywords
reverser
jets
reversed
thrust
blading
Prior art date
Application number
GR960400289T
Other languages
English (en)
Inventor
Felix Carimali
Michel Jean Lucien Legras
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9416827&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=GR3018892(T3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Hispano Suiza Sa filed Critical Hispano Suiza Sa
Publication of GR3018892T3 publication Critical patent/GR3018892T3/el

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/64Reversing fan flow
    • F02K1/70Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/56Reversing jet main flow
    • F02K1/563Reversing jet main flow in specified direction, e.g. to obviate its reinjection
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/56Reversing jet main flow
    • F02K1/60Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers

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)
  • Control Of Turbines (AREA)
  • Inverter Devices (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Coating By Spraying Or Casting (AREA)
GR960400289T 1991-09-11 1996-02-01 Thrust-reverser with improved guidance of the reversed jets. GR3018892T3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9111192A FR2681101B1 (fr) 1991-09-11 1991-09-11 Inverseur de poussee de turboreacteur a pilotage ameliore des nappes du flux inverse.

Publications (1)

Publication Number Publication Date
GR3018892T3 true GR3018892T3 (en) 1996-05-31

Family

ID=9416827

Family Applications (1)

Application Number Title Priority Date Filing Date
GR960400289T GR3018892T3 (en) 1991-09-11 1996-02-01 Thrust-reverser with improved guidance of the reversed jets.

Country Status (10)

Country Link
US (1) US5284015A (el)
EP (1) EP0534815B2 (el)
AT (1) ATE129779T1 (el)
CA (1) CA2077932C (el)
DE (1) DE69205791T3 (el)
ES (1) ES2079159T3 (el)
FR (1) FR2681101B1 (el)
GR (1) GR3018892T3 (el)
RU (1) RU2101534C1 (el)
WO (1) WO1993005291A1 (el)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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.
FR2706947B1 (el) * 1993-06-23 1995-07-28 Hispano Suiza Sa
FR2722534B1 (fr) * 1994-07-13 1996-08-14 Hispano Suiza Sa Inverseur de poussee de turboreacteur double flux, a obstacles externes
US5615834A (en) * 1995-01-31 1997-04-01 Osman; Medhat A. Ultra thrust reverser system
US5706649A (en) * 1995-04-03 1998-01-13 Boeing North American, Inc. Multi axis thrust vectoring for turbo fan engines
FR2736682B1 (fr) * 1995-07-12 1997-08-14 Hispano Suiza Sa Inverseur de poussee de turbomachine a double flux a portes dissymetriques
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
DE69521806D1 (de) * 1995-09-13 2001-08-23 Hurel Dubois Avions Strahlumkehrgitter für eine Schubumkehrvorrichtungsklappe
US5794433A (en) * 1996-06-18 1998-08-18 The Nordam Group, Inc. Thrust reverser door side fillers
FR2760789B1 (fr) * 1997-03-13 2001-09-07 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes a structure externe autoraidie
US5875995A (en) * 1997-05-20 1999-03-02 Rohr, Inc. Pivoting door type thrust reverser with deployable members for efflux control and flow separation
UA28120C2 (uk) * 1998-06-03 2000-10-16 Державне Підприємство "Запорізьке Машинобудівне Конструкторське Бюро "Прогрес" Імені Академіка О.Г.Івченка" Решітка аеродинамічних профілів пристрою реверсування тяги реактивного двигуна
RU2157906C2 (ru) * 1998-11-30 2000-10-20 Акционерное общество открытого типа "Казанское моторостроительное производственное объединение" Устройство для реверсирования тяги турбореактивного двигателя
FR2887301B1 (fr) * 2005-06-16 2007-08-31 Aircelle Sa Systeme de commande electronique pour nacelle
US8015797B2 (en) * 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
RU2356799C2 (ru) * 2007-07-30 2009-05-27 Алексей Алексеевич Комов Способ регулирования величины обратной тяги газотурбинных двигателей на пробеге двухдвигательного самолета при использовании реверса тяги
RU2372257C2 (ru) * 2007-07-30 2009-11-10 Алексей Алексеевич Комов Способ регулирования величины обратной тяги газотурбинных двигателей на пробеге четырехдвигательного самолета при использовании реверса тяги четырех двигателей
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
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
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US8052086B2 (en) * 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
FR2964704B1 (fr) * 2010-09-09 2016-04-01 Airbus Operations Sas Dispositif d'orientation de flux devie pour inverseur de poussee
WO2014074143A1 (en) * 2012-11-12 2014-05-15 United Technologies Corporation Aircraft with forward sweeping t-tail
RU2688642C1 (ru) * 2018-06-07 2019-05-21 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Реверсивное устройство турбореактивного двигателя
RU2768665C1 (ru) * 2021-10-13 2022-03-24 Сергей Иванович Ивандаев Способ реверсирования тяги двухконтурного газотурбинного двигателя и реверсивное устройство для его осуществления
US12276238B2 (en) * 2023-01-30 2025-04-15 The Boeing Company Multiple turn reverser with side turning vanes

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968150A (en) * 1958-02-21 1961-01-17 Rohr Aircraft Corp Jet engine exhaust sound suppressor and thrust reverser
FR1286178A (fr) * 1960-04-15 1962-03-02 Gen Electric Perfectionnements aux inverseurs de poussée
US3097484A (en) * 1960-06-13 1963-07-16 Thrust reversers for jet engines
US3283770A (en) * 1963-09-12 1966-11-08 Sperry Rand Corp Pneumatic reed relay
GB1002709A (en) * 1964-02-03 1965-08-25 Rolls Royce Improvements in or relating to thrust reversers for jet propulsion engines
FR1403761A (fr) * 1964-05-12 1965-06-25 Snecma Perfectionnement aux déviateurs de jet à grille d'aubes
FR1529361A (fr) * 1966-06-29 1968-06-14 Rolls Royce Dispositif inverseur de la poussée
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
US3640468A (en) * 1970-03-30 1972-02-08 Lockheed Aircraft Corp Thrust reverser for asymmetric exhaust efflux deflection
DE2252208C2 (de) * 1972-10-25 1974-02-07 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Schubumkehrvorrichtung
FR2348371A1 (fr) * 1976-04-14 1977-11-10 Astech Inverseur de poussee pour moteur a reaction
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
DE69205791D1 (de) 1995-12-07
ATE129779T1 (de) 1995-11-15
DE69205791T3 (de) 2001-06-07
DE69205791T2 (de) 1996-06-05
FR2681101A1 (fr) 1993-03-12
FR2681101B1 (fr) 1993-11-26
RU2101534C1 (ru) 1998-01-10
EP0534815B2 (fr) 2000-05-03
ES2079159T3 (es) 1996-01-01
CA2077932A1 (fr) 1993-03-12
EP0534815B1 (fr) 1995-11-02
CA2077932C (fr) 2000-01-18
EP0534815A1 (fr) 1993-03-31
US5284015A (en) 1994-02-08
WO1993005291A1 (fr) 1993-03-18

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