FR2992685B1 - Procede de commande d'une section de tuyere variable d'un aeronef - Google Patents

Procede de commande d'une section de tuyere variable d'un aeronef

Info

Publication number
FR2992685B1
FR2992685B1 FR1256305A FR1256305A FR2992685B1 FR 2992685 B1 FR2992685 B1 FR 2992685B1 FR 1256305 A FR1256305 A FR 1256305A FR 1256305 A FR1256305 A FR 1256305A FR 2992685 B1 FR2992685 B1 FR 2992685B1
Authority
FR
France
Prior art keywords
aircraft
controlling
pipe section
variable pipe
variable
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
FR1256305A
Other languages
English (en)
Other versions
FR2992685A1 (fr
Inventor
Pierre Caruel
Herve Hurlin
Olivier Kerbler
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
Priority to FR1256305A priority Critical patent/FR2992685B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to CN201380035244.7A priority patent/CN104411959A/zh
Priority to PCT/FR2013/051498 priority patent/WO2014006303A1/fr
Priority to EP13744642.3A priority patent/EP2867511A1/fr
Priority to CA 2877836 priority patent/CA2877836A1/fr
Priority to BR112014033049A priority patent/BR112014033049A2/pt
Priority to RU2015101781A priority patent/RU2015101781A/ru
Publication of FR2992685A1 publication Critical patent/FR2992685A1/fr
Priority to US14/584,435 priority patent/US10036348B2/en
Application granted granted Critical
Publication of FR2992685B1 publication Critical patent/FR2992685B1/fr
Active 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
    • F02K1/54—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
    • 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
    • F02K1/15—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/051—Thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Navigation (AREA)
FR1256305A 2012-07-02 2012-07-02 Procede de commande d'une section de tuyere variable d'un aeronef Active FR2992685B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1256305A FR2992685B1 (fr) 2012-07-02 2012-07-02 Procede de commande d'une section de tuyere variable d'un aeronef
PCT/FR2013/051498 WO2014006303A1 (fr) 2012-07-02 2013-06-27 Procédé de commande d'une section de tuyère variable d'un aéronef
EP13744642.3A EP2867511A1 (fr) 2012-07-02 2013-06-27 Procédé de commande d'une section de tuyère variable d'un aéronef
CA 2877836 CA2877836A1 (fr) 2012-07-02 2013-06-27 Procede de commande d'une section de tuyere variable d'un aeronef
CN201380035244.7A CN104411959A (zh) 2012-07-02 2013-06-27 用于控制航空器可变喷嘴截面的方法
BR112014033049A BR112014033049A2 (pt) 2012-07-02 2013-06-27 método para controlar uma posição de uma seção de bocal variável de uma aeronave
RU2015101781A RU2015101781A (ru) 2012-07-02 2013-06-27 Способ управления соплом переменного сечения летательного аппарата
US14/584,435 US10036348B2 (en) 2012-07-02 2014-12-29 Method for controlling a variable nozzle section of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1256305A FR2992685B1 (fr) 2012-07-02 2012-07-02 Procede de commande d'une section de tuyere variable d'un aeronef

Publications (2)

Publication Number Publication Date
FR2992685A1 FR2992685A1 (fr) 2014-01-03
FR2992685B1 true FR2992685B1 (fr) 2016-05-27

Family

ID=46785698

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1256305A Active FR2992685B1 (fr) 2012-07-02 2012-07-02 Procede de commande d'une section de tuyere variable d'un aeronef

Country Status (8)

Country Link
US (1) US10036348B2 (fr)
EP (1) EP2867511A1 (fr)
CN (1) CN104411959A (fr)
BR (1) BR112014033049A2 (fr)
CA (1) CA2877836A1 (fr)
FR (1) FR2992685B1 (fr)
RU (1) RU2015101781A (fr)
WO (1) WO2014006303A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106194494B (zh) * 2016-08-09 2018-01-05 南京理工大学 一种用于微型涡喷发动机加力燃烧室的可调喷管

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4106730A (en) * 1976-10-01 1978-08-15 The Boeing Company Engine out control system for STOL aircraft
US5706649A (en) * 1995-04-03 1998-01-13 Boeing North American, Inc. Multi axis thrust vectoring for turbo fan engines
FR2927309B1 (fr) * 2008-02-13 2010-04-16 Aircelle Sa Systeme de commande pour nacelle de turboreacteur
FR2930973B1 (fr) * 2008-05-06 2010-04-23 Airbus France Procede et dispositif de mise en oeuvre des inverseurs de poussee d'un aeronef
FR2932226B1 (fr) * 2008-06-06 2013-08-23 Aircelle Sa Procede de synchronisation des actionneurs d'un capot mobile d'inverseur de poussee
FR2958910B1 (fr) * 2010-04-20 2012-04-27 Aircelle Sa Nacelle pour moteur d'aeronef a tuyere de section variable
US8978356B2 (en) * 2010-12-03 2015-03-17 The Boeing Company Thrust reverser and variable area fan nozzle actuation system and method
US8713911B2 (en) * 2010-12-15 2014-05-06 Woodward Hrt, Inc. System and method for operating a thrust reverser for a turbofan propulsion system
EP2466102A1 (fr) * 2010-12-17 2012-06-20 Ecopra Dispositif de traitement d'un mélange gaz d'échappement/eau préalablement à son injection dans un moteur thermique et véhicule équipé d'un tel dispositif

Also Published As

Publication number Publication date
RU2015101781A (ru) 2016-08-20
WO2014006303A1 (fr) 2014-01-09
FR2992685A1 (fr) 2014-01-03
US10036348B2 (en) 2018-07-31
EP2867511A1 (fr) 2015-05-06
CA2877836A1 (fr) 2014-01-09
US20150108235A1 (en) 2015-04-23
CN104411959A (zh) 2015-03-11
BR112014033049A2 (pt) 2017-06-27

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