FR3005302B1 - Dispositif de commande de la puissance d'un moteur et d'un dispositif inverseur de poussee - Google Patents

Dispositif de commande de la puissance d'un moteur et d'un dispositif inverseur de poussee

Info

Publication number
FR3005302B1
FR3005302B1 FR1354140A FR1354140A FR3005302B1 FR 3005302 B1 FR3005302 B1 FR 3005302B1 FR 1354140 A FR1354140 A FR 1354140A FR 1354140 A FR1354140 A FR 1354140A FR 3005302 B1 FR3005302 B1 FR 3005302B1
Authority
FR
France
Prior art keywords
engine
controlling
power
thrust inverter
inverter device
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.)
Active
Application number
FR1354140A
Other languages
English (en)
Other versions
FR3005302A1 (fr
Inventor
Francois Munier
Hafid Elabellaoui
Philippe Savignac
Severin Viennot
Thierry Cartry
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 Electronics and Defense SAS
Original Assignee
Sagem Defense Securite 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 Sagem Defense Securite SA filed Critical Sagem Defense Securite SA
Priority to FR1354140A priority Critical patent/FR3005302B1/fr
Priority to EP14727880.8A priority patent/EP2976262A1/fr
Priority to US14/889,624 priority patent/US9422061B2/en
Priority to PCT/FR2014/051048 priority patent/WO2014181059A1/fr
Priority to CN201480025802.6A priority patent/CN105263804B/zh
Publication of FR3005302A1 publication Critical patent/FR3005302A1/fr
Application granted granted Critical
Publication of FR3005302B1 publication Critical patent/FR3005302B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64D31/00—Power plant control; Arrangement thereof
    • B64D31/02—Initiating means
    • B64D31/04—Initiating means actuated personally
    • 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
    • F02K1/54—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
FR1354140A 2013-05-06 2013-05-06 Dispositif de commande de la puissance d'un moteur et d'un dispositif inverseur de poussee Active FR3005302B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1354140A FR3005302B1 (fr) 2013-05-06 2013-05-06 Dispositif de commande de la puissance d'un moteur et d'un dispositif inverseur de poussee
EP14727880.8A EP2976262A1 (fr) 2013-05-06 2014-05-02 Dispositif de commande de la puissance d'un moteur et d'un dispositif inverseur de poussee
US14/889,624 US9422061B2 (en) 2013-05-06 2014-05-02 Device for controlling the power of an engine and for controlling a thrust reverser device
PCT/FR2014/051048 WO2014181059A1 (fr) 2013-05-06 2014-05-02 Dispositif de commande de la puissance d'un moteur et d'un dispositif inverseur de poussee
CN201480025802.6A CN105263804B (zh) 2013-05-06 2014-05-02 用于控制发动机功率和控制反推装置的装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1354140A FR3005302B1 (fr) 2013-05-06 2013-05-06 Dispositif de commande de la puissance d'un moteur et d'un dispositif inverseur de poussee

Publications (2)

Publication Number Publication Date
FR3005302A1 FR3005302A1 (fr) 2014-11-07
FR3005302B1 true FR3005302B1 (fr) 2015-06-05

Family

ID=49111345

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1354140A Active FR3005302B1 (fr) 2013-05-06 2013-05-06 Dispositif de commande de la puissance d'un moteur et d'un dispositif inverseur de poussee

Country Status (5)

Country Link
US (1) US9422061B2 (fr)
EP (1) EP2976262A1 (fr)
CN (1) CN105263804B (fr)
FR (1) FR3005302B1 (fr)
WO (1) WO2014181059A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9725182B2 (en) * 2009-10-06 2017-08-08 Safran Electronics & Defense Aircraft throttle control device including a cam coupling
US10676184B2 (en) 2014-08-28 2020-06-09 Sikorsky Aircraft Corporation Pitch control system for an aircraft
EP3186146B1 (fr) * 2014-08-28 2019-10-09 Sikorsky Aircraft Corporation Système de commande de pas
US10302044B2 (en) * 2015-12-18 2019-05-28 Rohr, Inc. Translating cascade thrust reverser with control of blocker door
US11124309B2 (en) 2018-01-09 2021-09-21 General Electric Company Single lever control system for engines with multiple control modes
CN111703586B (zh) * 2020-05-11 2023-05-30 中国南方航空股份有限公司 一种v2500发动机反推c涵道滑轨结构的更换方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3279184A (en) * 1964-07-15 1966-10-18 Boeing Co Control mechanism
US3572155A (en) * 1969-06-30 1971-03-23 Boeing Co Interlock mechanism
GB2116129A (en) * 1982-03-06 1983-09-21 Rolls Royce Anti-rotation lock
FR2860554B1 (fr) * 2003-10-06 2005-12-23 Hurel Hispano Verrou pour inverseur de poussee, muni d'un dispositif de blocage
FR2950861B1 (fr) * 2009-10-06 2011-10-28 Sagem Defense Securite Dispositif de commande des gaz d'un aeronef, incorporant une liaison par galet cranteur
US9725182B2 (en) * 2009-10-06 2017-08-08 Safran Electronics & Defense Aircraft throttle control device including a cam coupling
FR2950862B1 (fr) * 2009-10-06 2012-12-21 Sagem Defense Securite Dispositif de commande des gaz d'un aeronef, incorporant une liaison par cames

Also Published As

Publication number Publication date
CN105263804B (zh) 2017-04-12
CN105263804A (zh) 2016-01-20
FR3005302A1 (fr) 2014-11-07
WO2014181059A1 (fr) 2014-11-13
EP2976262A1 (fr) 2016-01-27
US9422061B2 (en) 2016-08-23
US20160083103A1 (en) 2016-03-24

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