FR3008071B1 - Nacelle de turboreacteur a tuyere variable - Google Patents

Nacelle de turboreacteur a tuyere variable

Info

Publication number
FR3008071B1
FR3008071B1 FR1356536A FR1356536A FR3008071B1 FR 3008071 B1 FR3008071 B1 FR 3008071B1 FR 1356536 A FR1356536 A FR 1356536A FR 1356536 A FR1356536 A FR 1356536A FR 3008071 B1 FR3008071 B1 FR 3008071B1
Authority
FR
France
Prior art keywords
turboboreacteur
vanable
nacelle
tube
vanable tube
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
FR1356536A
Other languages
English (en)
Other versions
FR3008071A1 (fr
Inventor
Olivier Kerbler
Olivier Gilo
Patrick Gonidec
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
Aircelle 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 Aircelle SA filed Critical Aircelle SA
Priority to FR1356536A priority Critical patent/FR3008071B1/fr
Priority to PCT/FR2014/051733 priority patent/WO2015001276A1/fr
Publication of FR3008071A1 publication Critical patent/FR3008071A1/fr
Priority to US14/987,302 priority patent/US10125721B2/en
Application granted granted Critical
Publication of FR3008071B1 publication Critical patent/FR3008071B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1207—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure
    • 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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1253—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a fixed structure and of a substantially axially movable external member
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • 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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • 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
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
FR1356536A 2013-07-04 2013-07-04 Nacelle de turboreacteur a tuyere variable Expired - Fee Related FR3008071B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1356536A FR3008071B1 (fr) 2013-07-04 2013-07-04 Nacelle de turboreacteur a tuyere variable
PCT/FR2014/051733 WO2015001276A1 (fr) 2013-07-04 2014-07-04 Nacelle de turboréacteur à tuyère variable
US14/987,302 US10125721B2 (en) 2013-07-04 2016-01-04 Nacelle for a turbojet engine with a variable nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1356536A FR3008071B1 (fr) 2013-07-04 2013-07-04 Nacelle de turboreacteur a tuyere variable

Publications (2)

Publication Number Publication Date
FR3008071A1 FR3008071A1 (fr) 2015-01-09
FR3008071B1 true FR3008071B1 (fr) 2017-07-28

Family

ID=49293687

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1356536A Expired - Fee Related FR3008071B1 (fr) 2013-07-04 2013-07-04 Nacelle de turboreacteur a tuyere variable

Country Status (3)

Country Link
US (1) US10125721B2 (fr)
FR (1) FR3008071B1 (fr)
WO (1) WO2015001276A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3033841B1 (fr) * 2015-03-17 2017-04-28 Aircelle Sa Inverseur de poussee pour nacelle de turboreacteur d’aeronef
FR3042226B1 (fr) * 2015-10-13 2019-06-07 Safran Nacelles Tuyere de section variable pour nacelle d'aeronef et nacelle pour un turboreacteur d'aeronef comportant une telle tuyere
GB201609071D0 (en) 2016-05-24 2016-07-06 Rolls Royce Plc Aircraft gas turbine engine nacelle
FR3054266B1 (fr) 2016-07-25 2018-08-31 Safran Nacelles Systeme d’actionnement d’un panneau de nacelle de turboreacteur
GB2564891A (en) 2017-07-26 2019-01-30 Short Brothers Plc Nacelle with thrust reverser
US20210108597A1 (en) * 2019-10-15 2021-04-15 General Electric Company Propulsion system architecture

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2976676A (en) * 1952-10-27 1961-03-28 Solar Aircraft Co Variable jet nozzle with coacting shroud
FR1514990A (fr) * 1966-09-07 1968-03-01 Snecma Tuyère à géométrie variable
US3599875A (en) * 1969-02-10 1971-08-17 United Aircraft Corp Translating air scoop ejector nozzle
US4141501A (en) * 1975-05-09 1979-02-27 Rolls-Royce (1971) Limited Nozzles for gas turbine engines
DE3619652C1 (en) * 1986-06-11 1990-10-11 Messerschmitt Boelkow Blohm Jet aircraft manoeuvring aid - has three movable flaps each suspended from four point linkage
US5117630A (en) * 1990-02-12 1992-06-02 Rohr Industries, Inc. Pivoting door thrust reverser
FR2934326A1 (fr) * 2008-07-28 2010-01-29 Aircelle Sa Dispositif d'inversion de poussee
FR2936222B1 (fr) 2008-09-24 2011-04-01 Aircelle Sa Nacelle a section de tuyere variable
FR2957979B1 (fr) 2010-03-25 2012-03-30 Aircelle Sa Dispositif d'inversion de poussee
FR2978802B1 (fr) 2011-08-05 2017-07-14 Aircelle Sa Inverseur a grilles mobiles et tuyere variable par translation

Also Published As

Publication number Publication date
FR3008071A1 (fr) 2015-01-09
US20160115902A1 (en) 2016-04-28
WO2015001276A1 (fr) 2015-01-08
US10125721B2 (en) 2018-11-13

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Legal Events

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Year of fee payment: 3

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Year of fee payment: 5

CD Change of name or company name

Owner name: SAFRAN NACELLES, FR

Effective date: 20180125

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Year of fee payment: 6

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Year of fee payment: 9

ST Notification of lapse

Effective date: 20230305