DE68902019T2 - Schubumkehrvorrichtung fuer ein zweikreistriebwerk mit beweglichen stroemungsleitklappen. - Google Patents

Schubumkehrvorrichtung fuer ein zweikreistriebwerk mit beweglichen stroemungsleitklappen.

Info

Publication number
DE68902019T2
DE68902019T2 DE8989402000T DE68902019T DE68902019T2 DE 68902019 T2 DE68902019 T2 DE 68902019T2 DE 8989402000 T DE8989402000 T DE 8989402000T DE 68902019 T DE68902019 T DE 68902019T DE 68902019 T2 DE68902019 T2 DE 68902019T2
Authority
DE
Germany
Prior art keywords
drawer
reverse
power plant
circuit power
flow valves
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
DE8989402000T
Other languages
English (en)
Other versions
DE68902019D1 (de
Inventor
Guy Bernard Vauchel
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 Nacelles 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 DE68902019D1 publication Critical patent/DE68902019D1/de
Publication of DE68902019T2 publication Critical patent/DE68902019T2/de
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)
DE8989402000T 1988-07-18 1989-07-12 Schubumkehrvorrichtung fuer ein zweikreistriebwerk mit beweglichen stroemungsleitklappen. Expired - Lifetime DE68902019T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8809671A FR2634251B1 (fr) 1988-07-18 1988-07-18 Inverseur de poussee de turboreacteur a double flux equipe de bords de deviation mobiles

Publications (2)

Publication Number Publication Date
DE68902019D1 DE68902019D1 (de) 1992-08-13
DE68902019T2 true DE68902019T2 (de) 1992-12-03

Family

ID=9368498

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8989402000T Expired - Lifetime DE68902019T2 (de) 1988-07-18 1989-07-12 Schubumkehrvorrichtung fuer ein zweikreistriebwerk mit beweglichen stroemungsleitklappen.

Country Status (5)

Country Link
US (1) US4976466A (de)
EP (1) EP0352171B1 (de)
CA (1) CA1327705C (de)
DE (1) DE68902019T2 (de)
FR (1) FR2634251B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011008917A1 (de) * 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinenschubumkehrvorrichtung
DE102011008919A1 (de) * 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinenschubumkehrvorrichtung

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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.
FR2680547B1 (fr) * 1991-08-21 1993-10-15 Hispano Suiza Inverseur de poussee de turboreacteur ayant un bord de deviation a courbure evolutive.
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.
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
FR2728626B1 (fr) 1994-12-21 1998-03-06 Hurel Dubois Avions Inverseur de poussee pour moteur a reaction a bord de deviation amenage
FR2740834B1 (fr) * 1995-11-02 1997-12-05 Hispano Suiza Sa Inverseur de poussee de turboreacteur a double flux muni de portes secondaires
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
EP0926333A1 (de) * 1997-12-26 1999-06-30 SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) Konfiguration einer Schubumkehrvorrichtung
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
FR2830051B1 (fr) * 2001-09-27 2003-11-07 Hurel Hispano Le Havre Systeme de verrouillage sur un inverseur de poussee a grilles
US8015797B2 (en) * 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
US7735778B2 (en) 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8052086B2 (en) 2007-11-16 2011-11-08 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
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
US8051639B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
FR2943749B1 (fr) * 2009-03-27 2011-03-04 Aircelle Sa Bielle coudee equipee d'au moins un moyen d'auto-alignement
US8951103B2 (en) * 2010-10-27 2015-02-10 Arzel Zoning Technology, Inc. Foldable, boot loadable, insertable air damper device
US9573690B2 (en) * 2011-09-06 2017-02-21 Honeywell International Inc. Thrust recovery outflow valve with a single bi-fold door and method of controlling aircraft cabin pressure
CN108661821B (zh) * 2017-03-31 2022-03-18 Mra系统有限责任公司 反推力器组件及操作方法
EP3851659B1 (de) * 2020-01-15 2022-08-17 Airbus Operations (S.A.S.) Kälteregelventil für ein wärmetauschersystem eines flugzeugantriebssystems

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1284851B (de) * 1967-07-26 1968-12-05 Ver Flugtechnische Werke Flugzeug mit zumindest einem Hubtriebwerk, dessen Auslass durch zwei hintereinanderliegende Klappen verschliessbar ist
GB1181746A (en) * 1968-06-19 1970-02-18 Rolls Royce Thrust Reverser for Jet Propulsion Plant
DE1920829C3 (de) * 1969-04-24 1974-03-07 Nissan Motor Co., Ltd., Yokohama (Japan) Selbstsperrendes Ausgleichsgetriebe für Kraftfahrzeuge
US3612401A (en) * 1970-01-29 1971-10-12 Rohr Corp Thrust-reversing apparatus for turbofan jet engine
US3747855A (en) * 1972-03-01 1973-07-24 Gen Electric Propulsion nozzles
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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011008917A1 (de) * 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinenschubumkehrvorrichtung
DE102011008919A1 (de) * 2011-01-19 2012-07-19 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinenschubumkehrvorrichtung
US9328694B2 (en) 2011-01-19 2016-05-03 Rolls-Royce Deutschland Ltd & Co Kg Aviation gas turbine thrust reversing device

Also Published As

Publication number Publication date
CA1327705C (fr) 1994-03-15
FR2634251A1 (fr) 1990-01-19
EP0352171A1 (de) 1990-01-24
FR2634251B1 (fr) 1993-08-13
US4976466A (en) 1990-12-11
DE68902019D1 (de) 1992-08-13
EP0352171B1 (de) 1992-07-08

Similar Documents

Publication Publication Date Title
DE68902019D1 (de) Schubumkehrvorrichtung fuer ein zweikreistriebwerk mit beweglichen stroemungsleitklappen.
DE69018693T2 (de) Kraftwerk mit kombiniertem Zyklus.
DE68912305D1 (de) Fluid-steuerungsmechanismus für kraftschaufeln.
DE3861588D1 (de) Absperrelement fuer ein ventil.
DE69206283D1 (de) Stromversorgung mit hohem Leistungsfaktor.
DE59102584D1 (de) Schubumkehrvorrichtung für ein propfantriebwerk.
DE68902727T2 (de) Schubumkehrvorrichtung fuer ein strahltriebwerk, ausgeruestet mit umkehrklappen mit strahlleitduesen.
DE68900042D1 (de) Strahl-mischer mit variablem durchtrittsquerschnitt fuer ein zweistromtriebwerk.
DE68906851D1 (de) Hydraulisches pilotventil.
DE3586157D1 (de) Schaltnetzteil mit mehreren ausgaengen.
IT8721269A0 (it) Valvola di controllo della pressione autoregolata.
DE58901320D1 (de) Stelleinrichtung fuer ein gaswechselventil.
DE58901579D1 (de) Stelleinrichtung fuer ein gaswechselventil.
DE3879300D1 (de) Gattersteuerungsanordnung fuer ein thyristorventil.
DE3863439D1 (de) Steuereinrichtung fuer ein ventil.
DE59103579D1 (de) Dampfumformventil mit Spindelantrieb.
DE68911285D1 (de) Ventilstellglied mit verbesserter Leistung.
DE69112893D1 (de) Solenoidservoventil mit variabler Öffnung für Servolenksystem mit variabler Unterstützung.
DE3889915D1 (de) Vorgesteuertes Dreiwegeventil.
DE69306870T2 (de) Hydraulisches Servoventil mit kontrollierter Abschaltung
DE68906972T2 (de) Stroemungssteuerventile.
DE68907685D1 (de) Steuerventil fuer fluid.
IT1208688B (it) Valvola a fungo in particolare azionata da valvola pilota
DE68922744D1 (de) Druckausgeglichenes dosierventil mit entlüftungsgesteuertem bypass.
DE58904194D1 (de) Gleichstromgespeiste steuerschaltung fuer ein magnetventil.

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: HISPANO-SUIZA AEROSTRUCTURES, GONFREVILLE L'ORCHER

8339 Ceased/non-payment of the annual fee