FR2937304B1 - Actionneur de gouverne d'aeronef a refroidissement statique. - Google Patents

Actionneur de gouverne d'aeronef a refroidissement statique.

Info

Publication number
FR2937304B1
FR2937304B1 FR0857030A FR0857030A FR2937304B1 FR 2937304 B1 FR2937304 B1 FR 2937304B1 FR 0857030 A FR0857030 A FR 0857030A FR 0857030 A FR0857030 A FR 0857030A FR 2937304 B1 FR2937304 B1 FR 2937304B1
Authority
FR
France
Prior art keywords
aircraft
static cooling
governor actuator
governor
actuator
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
FR0857030A
Other languages
English (en)
Other versions
FR2937304A1 (fr
Inventor
Alain Sagansan
Michel Todeschi
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 FR0857030A priority Critical patent/FR2937304B1/fr
Publication of FR2937304A1 publication Critical patent/FR2937304A1/fr
Application granted granted Critical
Publication of FR2937304B1 publication Critical patent/FR2937304B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/504—Transmitting means with power amplification using electrical energy using electro-hydrostatic actuators [EHA's]

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
FR0857030A 2008-10-16 2008-10-16 Actionneur de gouverne d'aeronef a refroidissement statique. Expired - Fee Related FR2937304B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0857030A FR2937304B1 (fr) 2008-10-16 2008-10-16 Actionneur de gouverne d'aeronef a refroidissement statique.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0857030A FR2937304B1 (fr) 2008-10-16 2008-10-16 Actionneur de gouverne d'aeronef a refroidissement statique.

Publications (2)

Publication Number Publication Date
FR2937304A1 FR2937304A1 (fr) 2010-04-23
FR2937304B1 true FR2937304B1 (fr) 2010-12-24

Family

ID=40810026

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0857030A Expired - Fee Related FR2937304B1 (fr) 2008-10-16 2008-10-16 Actionneur de gouverne d'aeronef a refroidissement statique.

Country Status (1)

Country Link
FR (1) FR2937304B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017154728A (ja) * 2016-02-29 2017-09-07 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 航空宇宙ビークルのための構造的に一体化された熱管理システム

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9016633B2 (en) * 2011-06-13 2015-04-28 The Boeing Company Electromechanical actuator (EMA) heat sink integrated de-icing system
US10723437B2 (en) 2017-05-30 2020-07-28 The Boeing Company System for structurally integrated thermal management for thin wing aircraft control surface actuators
CN112706913B (zh) * 2020-12-07 2022-03-11 沈阳飞机设计研究所扬州协同创新研究院有限公司 一种主动热控分布式电液伺服舵机

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5109672A (en) * 1990-01-16 1992-05-05 The Boeing Company Method and apparatus for cooling and replenishing aircraft hydraulic actuators
US6205803B1 (en) * 1996-04-26 2001-03-27 Mainstream Engineering Corporation Compact avionics-pod-cooling unit thermal control method and apparatus
US6938679B1 (en) * 1998-09-15 2005-09-06 The Boeing Company Heat transport apparatus
US6294853B1 (en) * 2000-08-02 2001-09-25 The United States Of America As Represented By The Secretary Of The Air Force Cooling of electromechanical actuator with phase change material and thermosyphons containing working fluid
JP2004144156A (ja) * 2002-10-23 2004-05-20 Sumitomo Heavy Ind Ltd 変速機の冷却構造、その冷却構造を有する変速機及び冷却方法
GB0523570D0 (en) * 2005-11-18 2005-12-28 Airbus Uk Ltd Aircraft cooling duct
DE102006012986A1 (de) * 2006-03-21 2007-09-27 Liebherr-Aerospace Lindenberg Gmbh Betätigungsvorrichtung
US8950468B2 (en) * 2007-05-11 2015-02-10 The Boeing Company Cooling system for aerospace vehicle components

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017154728A (ja) * 2016-02-29 2017-09-07 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 航空宇宙ビークルのための構造的に一体化された熱管理システム

Also Published As

Publication number Publication date
FR2937304A1 (fr) 2010-04-23

Similar Documents

Publication Publication Date Title
DE602006021127D1 (de) Turbinentriebwerk mit verbesserter Kühlung
FR2915179B1 (fr) Aeronef a impact environnemental reduit.
BRPI0818168A2 (pt) aerogerador com duas hélices sucessivas.
BRPI0817475A2 (pt) meio legível por computador.
DK2076675T3 (da) Mikroaktuator med voks
FR2909972B1 (fr) Aeronef a decollage vertical
FR2896537B1 (fr) Turbomachine a generateur-demarreur integre
FR2929482B1 (fr) Calculateur a l'agencement simplifie, destine a l'aeronautique
DE602007006263D1 (de) Turbomaschine
FR2967397B1 (fr) Dispositif de passage d'une helice en reverse comportant un actuateur agissant sur un maneton
FR2899200B1 (fr) Aeronef a impact environnemental reduit
DE502007001624D1 (de) Integriertes Motorkühlsystem
BRPI0817379A2 (pt) aeronave
BRPI0920992A2 (pt) atuador de movimento acionado.
DE602006021695D1 (de) Schnell ansprechender elektromagnetischer Aktuator
FI20110216L (fi) Polttoainepohjaisen säädön sisältävä moottorinohjausjärjestelmä
BRPI0922070A2 (pt) turbina.
BRPI0819600A2 (pt) Servoválvula.
NL2002312A1 (nl) Cooled turbine nozzle segment.
DK2220729T3 (da) Et aktuatorsystem
FR2929983B1 (fr) Secteur de distributeur de turbine de turbomachine.
DE602008002004D1 (de) Aktuatoranordnung
NL2002173A1 (nl) Synthetic Aviation Fuel.
FR2922192B1 (fr) Aeronef a double fuselage.
FR2937304B1 (fr) Actionneur de gouverne d'aeronef a refroidissement statique.

Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 8

ST Notification of lapse

Effective date: 20170630