ES2089635T3 - Inversor de empuje para motores a reaccion de aviones. - Google Patents

Inversor de empuje para motores a reaccion de aviones.

Info

Publication number
ES2089635T3
ES2089635T3 ES93108306T ES93108306T ES2089635T3 ES 2089635 T3 ES2089635 T3 ES 2089635T3 ES 93108306 T ES93108306 T ES 93108306T ES 93108306 T ES93108306 T ES 93108306T ES 2089635 T3 ES2089635 T3 ES 2089635T3
Authority
ES
Spain
Prior art keywords
push
reaction engines
aircraft reaction
define
push inverter
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
ES93108306T
Other languages
English (en)
Inventor
Alfredo Gatti
Luigi Gerbi
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.)
Leonardo SpA
Original Assignee
Finmeccanica SpA
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 Finmeccanica SpA filed Critical Finmeccanica SpA
Application granted granted Critical
Publication of ES2089635T3 publication Critical patent/ES2089635T3/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
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/11—Varying effective area of jet pipe or nozzle by means of pivoted eyelids

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Exhaust Silencers (AREA)
  • Control Of Turbines (AREA)

Abstract

SE PRESENTA UN DISPOSITIVO DE INVERSION DEL EMPUJE PARA MOTORES DE AVIONES A REACCION, EL DISPOSITIVO COMPRENDE UN PAR DE SEMICUBIERTAS (5) QUE PUEDEN MOVERSE ENTRE UNA POSICION CONTRAIDA EN LA QUE DEFINEN UNA PARTE DE LA TOBERA DE SALIDA (1) Y UNA POSICION DESPLEGADA EN LA QUE DEFINEN UNA DEFLEXION PARA LA INVERSION DEL EMPUJE Y UN CUELLO FINAL (9) INSTALADOS EN LA TERMINACION DE LA TOBERA DE SALIDA (1) DE MANERA QUE SE MUEVA ENTRE UNA POSICION AVANZADA, EN LA QUE DICHO CUELLO, DEFINE EL FINAL DE LA TOBERA DE DESCARGA FORMANDO UNA TOBERA DE DESCARGA DE FORMA IDEAL, Y UNA POSICION RETRAIDA QUE PERMITE EL DESPLIEGUE DE DICHAS SEMICUBIERTAS (5).
ES93108306T 1992-06-09 1993-05-22 Inversor de empuje para motores a reaccion de aviones. Expired - Lifetime ES2089635T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITTO920490A IT1257222B (it) 1992-06-09 1992-06-09 Dispositivo inversore di spinta per motori aeronautici a getto.

Publications (1)

Publication Number Publication Date
ES2089635T3 true ES2089635T3 (es) 1996-10-01

Family

ID=11410523

Family Applications (1)

Application Number Title Priority Date Filing Date
ES93108306T Expired - Lifetime ES2089635T3 (es) 1992-06-09 1993-05-22 Inversor de empuje para motores a reaccion de aviones.

Country Status (6)

Country Link
US (1) US5392991A (es)
EP (1) EP0574730B1 (es)
JP (1) JP2640207B2 (es)
DE (1) DE69301503T2 (es)
ES (1) ES2089635T3 (es)
IT (1) IT1257222B (es)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2717860B1 (fr) * 1994-03-28 1996-05-31 Sud Ouest Conception Aeronauti Inverseur de poussée doté d'au moins une porte basculante, pour moteur à réaction, notamment d'aéronef, et moteur à réaction équipé de cet inverseur de poussée.
DE69512616T2 (de) * 1994-12-15 2000-06-29 Dee Howard Co Schubumkehrvorrichtung mit in Längsrichtung verschiebbaren Klappen
FR2734868B1 (fr) * 1995-06-02 1997-08-14 Hurel Dubois Avions Ensemble d'inverseur de poussee a deux portes
FR2741114B1 (fr) * 1995-11-15 1997-12-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a obstacles aval tendant a l'equilibrage
FR2768773B1 (fr) * 1997-09-25 1999-11-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a coquilles internes
FR2788564B1 (fr) * 1999-01-14 2001-02-16 Snecma Tuyere d'ejection de turboreacteur a reverse integree
FR2887854B1 (fr) * 2005-06-30 2008-08-08 Airbus France Sas Nacelle pour aeronef et aeronef muni d'au moins une telle nacelle
US8015797B2 (en) * 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
FR2912189B1 (fr) * 2007-02-01 2012-02-17 Airbus France Nacelle d'aeronef incorporant un dispositif pour inverser la poussee
FR2914956A1 (fr) * 2007-04-12 2008-10-17 Aircelle Sa Nacelle pour turboreacteur equipee d'un systeme d'inversion de poussee a porte
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
US8002217B2 (en) * 2007-11-16 2011-08-23 Spirit Aerosystems, Inc. System for adjustment of thrust reverser pivot door
US8052086B2 (en) 2007-11-16 2011-11-08 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
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8434715B2 (en) * 2009-07-30 2013-05-07 Jean-Pierre Lair Nested fairing thrust reverser
US10040563B1 (en) * 2013-04-11 2018-08-07 Geoffrey P. Pinto Dual panel actuator system for jet engines
FR3006378B1 (fr) * 2013-05-29 2015-05-15 Aircelle Sa Nacelle de turboreacteur comportant un dispositif d'inversion de pousse a portes, comprenant des flancs interieurs sur les cotes de l'ouverture
US9388768B2 (en) * 2013-08-23 2016-07-12 Rohr, Inc. Blocker door actuation system and apparatus
RU2663249C1 (ru) 2017-03-16 2018-08-03 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Способ изготовления секций несущей решетки реверсера тяги
US11300077B2 (en) 2018-10-02 2022-04-12 Rohr, Inc. Deployable fairing for door reversers systems and methods
EP3620643B1 (en) * 2018-09-06 2021-10-27 Rohr, Inc. Deployable fairing for door reversers systems and methods
US11333102B2 (en) 2018-09-06 2022-05-17 Rohr, Inc. Thrust reverser actuation arrangement and deployable fairing systems and methods
US11346304B2 (en) 2018-09-06 2022-05-31 Rohr, Inc. Thrust reverser single degree of freedom actuator mechanism systems and methods
FR3092874B1 (fr) * 2019-02-14 2021-01-22 Safran Nacelles Système de fermeture de portes pour inverseur de poussée d’une nacelle d’aéronef
US20240035427A1 (en) * 2022-08-01 2024-02-01 Rohr, Inc. Thrust reverser cascade with offset vane leading edges

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2680948A (en) * 1948-08-30 1954-06-15 Engineering & Res Corp Variable area tail pipe for jet engines
GB800770A (en) * 1955-03-10 1958-09-03 Havilland Engine Co Ltd Nozzle assemblies for jet propulsion apparatus
GB1130268A (en) * 1967-07-01 1968-10-16 Rolls Royce Improvements in or relating to gas turbine by-pass engines
US3532275A (en) * 1967-11-09 1970-10-06 Rohr Corp Jet reverser drive system
GB1288834A (es) * 1970-03-14 1972-09-13
FR2382593A1 (fr) * 1977-03-04 1978-09-29 Hurel Dubois Avions Dispositif pour la commande d'un inverseur de poussee pour moteur a reaction
GB2182724B (en) * 1985-10-08 1988-12-07 Rolls Royce Gas turbine engine thrust reverser
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
US4966327A (en) * 1988-10-27 1990-10-30 The Dee Howard Company Jet engine provided with a thrust reverser
FR2638783B1 (fr) * 1988-11-10 1991-04-05 Astech Inverseur de poussee notamment pour moteur a reaction d'aeronef
US5176340A (en) * 1991-11-26 1993-01-05 Lair Jean Pierre Thrust reverser with a planar exit opening

Also Published As

Publication number Publication date
IT1257222B (it) 1996-01-10
DE69301503T2 (de) 1996-07-18
EP0574730A1 (en) 1993-12-22
JPH06193508A (ja) 1994-07-12
US5392991A (en) 1995-02-28
JP2640207B2 (ja) 1997-08-13
ITTO920490A0 (it) 1992-06-09
EP0574730B1 (en) 1996-02-07
ITTO920490A1 (it) 1993-12-09
DE69301503D1 (de) 1996-03-21

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