FR2715695B1 - Inverseur de poussée pour un moteur à turbine à gaz à soufflante canalisée. - Google Patents

Inverseur de poussée pour un moteur à turbine à gaz à soufflante canalisée.

Info

Publication number
FR2715695B1
FR2715695B1 FR9500527A FR9500527A FR2715695B1 FR 2715695 B1 FR2715695 B1 FR 2715695B1 FR 9500527 A FR9500527 A FR 9500527A FR 9500527 A FR9500527 A FR 9500527A FR 2715695 B1 FR2715695 B1 FR 2715695B1
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
thrust reverser
ducted fan
ducted
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 - Fee Related
Application number
FR9500527A
Other languages
English (en)
Other versions
FR2715695A1 (fr
Inventor
Arnold Charles Newton
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2715695A1 publication Critical patent/FR2715695A1/fr
Application granted granted Critical
Publication of FR2715695B1 publication Critical patent/FR2715695B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K1/76—Control or regulation of thrust 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
    • F02K1/54—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

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)
FR9500527A 1994-02-01 1995-01-18 Inverseur de poussée pour un moteur à turbine à gaz à soufflante canalisée. Expired - Fee Related FR2715695B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9401836A GB2285958B (en) 1994-02-01 1994-02-01 Thrust reverser for a ducted fan gas turbine engine

Publications (2)

Publication Number Publication Date
FR2715695A1 FR2715695A1 (fr) 1995-08-04
FR2715695B1 true FR2715695B1 (fr) 1997-06-20

Family

ID=10749625

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9500527A Expired - Fee Related FR2715695B1 (fr) 1994-02-01 1995-01-18 Inverseur de poussée pour un moteur à turbine à gaz à soufflante canalisée.

Country Status (3)

Country Link
US (1) US5598701A (fr)
FR (1) FR2715695B1 (fr)
GB (1) GB2285958B (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2737256B1 (fr) * 1995-07-26 1997-10-17 Aerospatiale Turboreacteur a double flux a portes d'inversion de poussee non soumises au flux secondaire dans leur position inactive
US5987880A (en) * 1997-07-08 1999-11-23 Mcdonnell Douglas Corporation Supersonic engine, multi-port thrust reversing system
US6311928B1 (en) 2000-01-05 2001-11-06 Stage Iii Technologies, L.C. Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor
FR2887854B1 (fr) * 2005-06-30 2008-08-08 Airbus France Sas Nacelle pour aeronef et aeronef muni d'au moins une telle nacelle
US8413932B2 (en) * 2010-04-10 2013-04-09 Aerofex, Inc. Peripheral control ejector
US10040563B1 (en) * 2013-04-11 2018-08-07 Geoffrey P. Pinto Dual panel actuator system for jet engines

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
US3640640A (en) * 1970-12-04 1972-02-08 Rolls Royce Fluid flow machine
US3815357A (en) * 1971-01-28 1974-06-11 Rohr Industries Inc Thrust reversing apparatus
US3736750A (en) * 1971-03-12 1973-06-05 Rolls Royce Power plant
SE396135B (sv) * 1972-07-31 1977-09-05 Bofors Ab Styranordning for raketmotordrivna projektiler
US3907224A (en) * 1973-06-01 1975-09-23 Boeing Co Variable ramp exhaust nozzle and clamshell reverser
US3844482A (en) * 1973-06-01 1974-10-29 Boeing Co Variable ramp exhaust nozzle and clamshell reverser
FR2337258A1 (fr) * 1976-01-03 1977-07-29 Plessey Handel Investment Ag Equipement inverseur de poussee pour moteurs a double flux
GB1534583A (en) * 1976-06-08 1978-12-06 Short Bros Ltd Reversal of thrust in gas turbine engines
GB2080486B (en) * 1980-07-15 1984-02-15 Rolls Royce Shafts
FR2529976B1 (fr) * 1982-07-08 1986-11-28 Hispano Suiza Sa Dispositif de desaccouplage de deux machines tournantes

Also Published As

Publication number Publication date
FR2715695A1 (fr) 1995-08-04
GB2285958B (en) 1997-12-10
US5598701A (en) 1997-02-04
GB9401836D0 (en) 1994-03-30
GB2285958A (en) 1995-08-02

Similar Documents

Publication Publication Date Title
DE69611506T2 (de) Schubumkehrvorrichtung mit Sekundärklappen für ein Bläsertriebwerk
GB2226995B (en) Gas turbine jet engine having a thrust reverser.
DE69004636D1 (de) Schubumkehrvorrichtung für ein Strahltriebwerk.
DE69602296D1 (de) Schubumkehrvorrichtung für ein Bläsertriebwerk
FR2752879B1 (fr) Joints annulaires a air pour moteur a turbine a gaz
NL194700B (nl) Axiale stromingsturbine voor een gasturbinemotor.
GB2247522B (en) Gas turbine engine combustor
GB2320526B (en) Ducted fan gas turbine engine
DE69301503D1 (de) Schubumkehrvorrichtung für ein Strahltriebwerk
DE69714949D1 (de) Elektrisches Steuerungssystem für die Schubumkehrvorrichtung eines Turbotriebwerkes
NL194734B (nl) Gekoeld turbineblad voor een gasturbinemotor.
FR2594886B1 (fr) Module propulsif pour un moteur aeronautique a turbine a gaz
GB9018014D0 (en) Gas turbine engine combustor
GB9018013D0 (en) Gas turbine engine combustor
DE69714565T2 (de) Schubumkehrvorrichtung für ein Strahltriebwerk mit Klappe am Hinterteil
DE59504264D1 (de) Brennkammer für eine gasturbine
GB2288639B (en) Ducted fan gas turbine engine nacelle assembly
IT1240296B (it) Assieme rotorico per turbomotore a gas
EP0466316A3 (en) Gas turbine engine thrust reverser control
DE69610272T2 (de) Schubumkehrvorrichtung für ein Strahltriebwerk, mit einer Klappe
DE69717344D1 (de) Klappen mit Leitflächen für eine Schubumkehrvorrichtung eines Bläsertriebwerkes
DE69412755T2 (de) Schubumkehrvorrichtung für ein Bläsertriebwerk
GB9106515D0 (en) Device for operation of a gas turbine engine thrust reverser system
FR2715695B1 (fr) Inverseur de poussée pour un moteur à turbine à gaz à soufflante canalisée.
GB9119852D0 (en) Ducted fan gas turbine engine accessory drive system

Legal Events

Date Code Title Description
ST Notification of lapse