FR2088393A1 - - Google Patents

Info

Publication number
FR2088393A1
FR2088393A1 FR7116395A FR7116395A FR2088393A1 FR 2088393 A1 FR2088393 A1 FR 2088393A1 FR 7116395 A FR7116395 A FR 7116395A FR 7116395 A FR7116395 A FR 7116395A FR 2088393 A1 FR2088393 A1 FR 2088393A1
Authority
FR
France
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.)
Pending
Application number
FR7116395A
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.)
MINI AVIAT SUPPLY
Original Assignee
MINI AVIAT SUPPLY
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 MINI AVIAT SUPPLY filed Critical MINI AVIAT SUPPLY
Publication of FR2088393A1 publication Critical patent/FR2088393A1/fr
Pending 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
    • 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
    • F02K1/563—Reversing jet main flow in specified direction, e.g. to obviate its reinjection
    • 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
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
FR7116395A 1970-05-06 1971-05-06 Pending FR2088393A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2181070 1970-05-06

Publications (1)

Publication Number Publication Date
FR2088393A1 true FR2088393A1 (fr) 1972-01-07

Family

ID=10169203

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7116395A Pending FR2088393A1 (fr) 1970-05-06 1971-05-06

Country Status (4)

Country Link
US (1) US3717304A (fr)
DE (1) DE2122005A1 (fr)
FR (1) FR2088393A1 (fr)
IT (1) IT945912B (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2327411A1 (fr) * 1975-10-11 1977-05-06 Rolls Royce Perfectionnements aux inverseurs de poussee pour turboreacteurs a soufflante canalisee
FR2559838A1 (fr) * 1984-02-21 1985-08-23 Hurel Dubois Avions Procede et dispositif permettant le controle du jet inverse dans les moteurs a reaction a inverseur de poussee
FR2983173A1 (fr) * 2011-11-24 2013-05-31 Aircelle Sa Actionneur pour nacelle de turboreacteur d'aeronef a partie arriere notamment annulaire monobloc
US20160245230A1 (en) * 2015-02-23 2016-08-25 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6568172B2 (en) * 2001-09-27 2003-05-27 The Nordam Group, Inc. Converging nozzle thrust reverser
FR2922958B1 (fr) * 2007-10-25 2009-11-20 Aircelle Sa Inverseur de poussee a grilles
FR2956162B1 (fr) * 2010-02-08 2012-11-16 Snecma Tuyere de flux froid d'un turboreacteur a double flux a flux separes incorporant un inverseur de poussee a grilles
US10145335B2 (en) * 2012-09-28 2018-12-04 United Technologies Corporation Turbomachine thrust reverser
DE102015206093A1 (de) * 2015-04-02 2016-10-06 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung einer Fluggasturbine
US10648426B2 (en) 2016-01-14 2020-05-12 Honeywell International Inc. Single row vane assembly for a thrust reverser
US10337454B2 (en) 2016-01-25 2019-07-02 Honeywell International Inc. Thrust reverser with asymmetric vane geometry
US20230408091A1 (en) * 2022-06-21 2023-12-21 General Electric Company Cowl assembly for a gas turbine engine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3262268A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
US3262269A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
US3262271A (en) * 1965-07-30 1966-07-26 Gen Electric Thrust reverser

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2327411A1 (fr) * 1975-10-11 1977-05-06 Rolls Royce Perfectionnements aux inverseurs de poussee pour turboreacteurs a soufflante canalisee
FR2559838A1 (fr) * 1984-02-21 1985-08-23 Hurel Dubois Avions Procede et dispositif permettant le controle du jet inverse dans les moteurs a reaction a inverseur de poussee
FR2983173A1 (fr) * 2011-11-24 2013-05-31 Aircelle Sa Actionneur pour nacelle de turboreacteur d'aeronef a partie arriere notamment annulaire monobloc
WO2013093256A1 (fr) * 2011-11-24 2013-06-27 Aircelle Nacelle de turboreacteur d'aeronef a partie arriere notamment annulaire monobloc et actionneur
CN103958349A (zh) * 2011-11-24 2014-07-30 埃尔塞乐公司 用于特别地具有一体式环形后部的飞机涡轮发动机舱的致动器
CN103958349B (zh) * 2011-11-24 2016-12-07 埃尔塞乐公司 用于特别地具有一体式环形后部的飞机涡轮发动机舱的致动器
US10047634B2 (en) 2011-11-24 2018-08-14 Aircelle Actuator for aircraft turbine engine nacelle with notably one-piece annular rear part
US20160245230A1 (en) * 2015-02-23 2016-08-25 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle
US10151270B2 (en) * 2015-02-23 2018-12-11 Rolls-Royce Deutschland Ltd & Co Kg Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzle

Also Published As

Publication number Publication date
IT945912B (it) 1973-05-10
DE2122005A1 (de) 1972-02-17
US3717304A (en) 1973-02-20

Similar Documents

Publication Publication Date Title
AR204384A1 (fr)
FR2088393A1 (fr)
ATA96471A (fr)
AU1473870A (fr)
AU1146470A (fr)
AU465380B2 (fr)
AU2017870A (fr)
AU1336970A (fr)
AU1326870A (fr)
AU2085370A (fr)
AU1833270A (fr)
AU1716970A (fr)
AU1517670A (fr)
AR195465A1 (fr)
AU1832970A (fr)
AU1841070A (fr)
AU2144270A (fr)
AU1918570A (fr)
AU1247570A (fr)
AU1603270A (fr)
AU1689770A (fr)
AU1872870A (fr)
AU1789870A (fr)
AU1277070A (fr)
AU1591370A (fr)

Legal Events

Date Code Title Description
TP Transmission of property