FR3005489B1 - Dispositif de commande d'une tuyere a section variable d'un aeronef - Google Patents

Dispositif de commande d'une tuyere a section variable d'un aeronef

Info

Publication number
FR3005489B1
FR3005489B1 FR1354201A FR1354201A FR3005489B1 FR 3005489 B1 FR3005489 B1 FR 3005489B1 FR 1354201 A FR1354201 A FR 1354201A FR 1354201 A FR1354201 A FR 1354201A FR 3005489 B1 FR3005489 B1 FR 3005489B1
Authority
FR
France
Prior art keywords
aircraft
controlling
variable section
section tube
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
FR1354201A
Other languages
English (en)
Other versions
FR3005489A1 (fr
Inventor
Guillaume Bulin
Armand Ruggeri
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1354201A priority Critical patent/FR3005489B1/fr
Priority to US14/269,815 priority patent/US9657685B2/en
Priority to CN201410189843.0A priority patent/CN104141554B/zh
Publication of FR3005489A1 publication Critical patent/FR3005489A1/fr
Application granted granted Critical
Publication of FR3005489B1 publication Critical patent/FR3005489B1/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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
    • 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
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • 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
    • 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
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • 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
    • F05D2260/00—Function
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • F05D2260/57—Kinematic linkage, i.e. transmission of position using servos, independent actuators, etc.
    • 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
    • F05D2260/00—Function
    • F05D2260/84—Redundancy
    • 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
    • F05D2260/00—Function
    • F05D2260/90—Braking
    • F05D2260/902—Braking using frictional mechanical forces
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Multiple Motors (AREA)
  • Control Of Position Or Direction (AREA)
FR1354201A 2013-05-07 2013-05-07 Dispositif de commande d'une tuyere a section variable d'un aeronef Expired - Fee Related FR3005489B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1354201A FR3005489B1 (fr) 2013-05-07 2013-05-07 Dispositif de commande d'une tuyere a section variable d'un aeronef
US14/269,815 US9657685B2 (en) 2013-05-07 2014-05-05 Device for controlling a nozzle of variable cross-section of an aircraft
CN201410189843.0A CN104141554B (zh) 2013-05-07 2014-05-07 用于控制航空器的具有可变横截面的喷嘴的装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1354201A FR3005489B1 (fr) 2013-05-07 2013-05-07 Dispositif de commande d'une tuyere a section variable d'un aeronef

Publications (2)

Publication Number Publication Date
FR3005489A1 FR3005489A1 (fr) 2014-11-14
FR3005489B1 true FR3005489B1 (fr) 2017-03-17

Family

ID=48782476

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1354201A Expired - Fee Related FR3005489B1 (fr) 2013-05-07 2013-05-07 Dispositif de commande d'une tuyere a section variable d'un aeronef

Country Status (3)

Country Link
US (1) US9657685B2 (fr)
CN (1) CN104141554B (fr)
FR (1) FR3005489B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110823578A (zh) * 2019-10-25 2020-02-21 中国航发北京航科发动机控制系统科技有限公司 一种航空发动机喷嘴的模拟试验装置
CN111852685B (zh) * 2020-05-25 2021-09-24 北京动力机械研究所 一种直线运动构件的指定极限位置限制装置

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2986003A (en) * 1957-04-04 1961-05-30 Napier & Son Ltd Fuel supply systems for compound ramjet-turborocket engines
US3814537A (en) * 1972-09-22 1974-06-04 Gen Motors Corp Turbine nozzle control
FR2444505A1 (fr) 1978-12-22 1980-07-18 Air Ind Procede et dispositif de deplacement alternatif d'appareils automatiques de projection de produits de revetement
US4985666A (en) 1988-08-30 1991-01-15 Sony Corporation Safety device for video cassette recorder
US5467613A (en) 1994-04-05 1995-11-21 Carrier Corporation Two phase flow turbine
JPH09195853A (ja) 1995-12-14 1997-07-29 United Technol Corp <Utc> 可変面積ファンエキゾーストノズル
US6439504B1 (en) 2001-06-15 2002-08-27 Honeywell International, Inc. System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system
US6684623B2 (en) * 2002-02-27 2004-02-03 Honeywell International, Inc. Gearless electric thrust reverser actuators and actuation system incorporating same
US7127880B2 (en) * 2003-08-29 2006-10-31 The Nordam Group, Inc. Induction coupled variable nozzle
FR2925607B1 (fr) * 2007-12-21 2013-05-10 Aircelle Sa Nacelle pour moteur d'aeronef a tuyere de section variable
FR2927309B1 (fr) 2008-02-13 2010-04-16 Aircelle Sa Systeme de commande pour nacelle de turboreacteur
EP2239449B1 (fr) * 2009-04-06 2015-09-30 Rohr, Inc. Ensemble de nacelle pour moteurs d'avion à réacteur à double flux
GB201002315D0 (en) * 2010-02-11 2010-03-31 Goodrich Actuation Systems Ltd Control system
FR2960600B1 (fr) * 2010-06-01 2013-10-25 Aircelle Sa Systeme d'actionnement d'un dispositif d'inversion de poussee
FR2960917B1 (fr) * 2010-06-03 2012-05-18 Aircelle Sa Inverseur de poussee a section de tuyere variable verrouillable
US20120139531A1 (en) * 2010-12-07 2012-06-07 Hamilton Sundstrand Corporation Position detecting system
US8615982B2 (en) * 2011-07-05 2013-12-31 Hamilton Sundstrand Corporation Integrated electric variable area fan nozzle thrust reversal actuation system
FR3005488B1 (fr) 2013-05-07 2015-05-29 Airbus Operations Sas Dispositif de commande d'une tuyere a section variable d'un aeronef

Also Published As

Publication number Publication date
CN104141554A (zh) 2014-11-12
US20160003188A1 (en) 2016-01-07
US9657685B2 (en) 2017-05-23
CN104141554B (zh) 2017-07-11
FR3005489A1 (fr) 2014-11-14

Similar Documents

Publication Publication Date Title
FR3011815B1 (fr) Dispositif de commande de vol d&#39;un aeronef
FR3018025B1 (fr) Dispositif de commande d&#39;un haut-parleur
FR3018024B1 (fr) Dispositif de commande d&#39;un haut-parleur
FR3028062B1 (fr) Dispositif d&#39;interface de commande capacitif integre a un ecran d&#39;affichage
FR3014348B1 (fr) Dispositif de commande a retour d&#39;effort multidirectionnel
FR3004628B3 (fr) Dispositif de reglage d&#39;un panneau de tiroir
FR3014531B1 (fr) Dispositif de fixation pour cable
FR3010387B1 (fr) Aeronef comprenant un dispositif de commande d&#39;une tuyere a section variable alimente par deux alimentations electriques independantes
FR3035165B1 (fr) &#34;dispositif de commande impulsionnelle d&#39;une boite de vitesses automatique&#34;
FR3006904B1 (fr) Dispositif de lancement pour aeronef commande a distance
FR3005992B1 (fr) Dispositif de passage de servitudes pour une turbomachine
PL2941615T3 (pl) Osłona przeciwświetlna o zmiennej długości dla czujnika elektrooptycznego wewnątrz dziobu pojazdu
FR3005489B1 (fr) Dispositif de commande d&#39;une tuyere a section variable d&#39;un aeronef
FR3033767B1 (fr) Dispositif de commande de vol d&#39;un aeronef
FR2994220B1 (fr) Dispositif de commande d&#39;une tuyere a section variable d&#39;un aeronef
FR3027635B1 (fr) Systeme de commande d&#39;aubes a calage variable pour une turbomachine
FR3015705B1 (fr) Procede de parametrage d&#39;une unite de commande d&#39;un equipement domotique
FR3005488B1 (fr) Dispositif de commande d&#39;une tuyere a section variable d&#39;un aeronef
FR3042775B1 (fr) Dispositif de commande de vol d&#39;un aeronef
FR2989429B1 (fr) Dispositif de commande d&#39;une tuyere a section variable d&#39;un aeronef
FR3039966B1 (fr) Dispositif de formation d&#39;un andain
FR3033384B1 (fr) Dispositif de commande hydraulique
FR3001553B1 (fr) Dispositif de commande pour un systeme d&#39;automatisme
FR3018771B1 (fr) Aeronef muni d&#39;un systeme avionique
FR3011034B1 (fr) Dispositif de limitation de jeu pour turbomachine

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

ST Notification of lapse

Effective date: 20210105