BRPI0517110A - dispositivo para emitir um sinal de autorização, sistema para controlar pelo menos um motor de aeronave e aeronave - Google Patents

dispositivo para emitir um sinal de autorização, sistema para controlar pelo menos um motor de aeronave e aeronave

Info

Publication number
BRPI0517110A
BRPI0517110A BRPI0517110-5A BRPI0517110A BRPI0517110A BR PI0517110 A BRPI0517110 A BR PI0517110A BR PI0517110 A BRPI0517110 A BR PI0517110A BR PI0517110 A BRPI0517110 A BR PI0517110A
Authority
BR
Brazil
Prior art keywords
aircraft
issuing
engine
controlling
authorization signal
Prior art date
Application number
BRPI0517110-5A
Other languages
English (en)
Inventor
Patrick Zaccaria
Marie-Pierre Fuertes
Original Assignee
Airbus France
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 France filed Critical Airbus France
Publication of BRPI0517110A publication Critical patent/BRPI0517110A/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F02C9/285—Mechanical command devices linked to the throttle lever
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/56—Control of fuel supply conjointly with another control of the plant with power transmission 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
    • F05D2260/00—Function
    • F05D2260/80—Diagnostics

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Traffic Control Systems (AREA)

Abstract

DISPOSITIVO PARA EMITIR UM SINAL DE AUTORIZAçãO, SISTEMA PARA CONTROLAR PELO MENOS UM MOTOR DE AERONAVE E AERONAVE. A invenção se refere a um dispositivo (1) compreendendo um primeiro meio (4, 10) para determinar parâmetros particulares com respeito a uma aeronave, incluindo a posição de uma alavanca de aceleração para controlar alimentação de combustível para o motor, e um segundo meio (11) para determinar, com base nos citados parâmetros particulares, se a aeronave se encontra em um estado que autorize uma ação sobre as condições operacionais do motor e para emitir, se for o caso, o correspondente sinal de autorização.
BRPI0517110-5A 2004-12-20 2005-12-12 dispositivo para emitir um sinal de autorização, sistema para controlar pelo menos um motor de aeronave e aeronave BRPI0517110A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0413553A FR2879562B1 (fr) 2004-12-20 2004-12-20 Dispositif pour emettre une autorisation d'agir sur le fonctionnement d'un moteur d'aeronef et systeme de controle de moteur comportant un tel dispositif
PCT/FR2005/003100 WO2006067295A1 (fr) 2004-12-20 2005-12-12 Dispositif pour emettre une autorisation d'agir sur le fonctionnement d'un moteur d'aeronef et systeme de controle de moteur comportant un tel dispositif

Publications (1)

Publication Number Publication Date
BRPI0517110A true BRPI0517110A (pt) 2008-09-30

Family

ID=34952627

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0517110-5A BRPI0517110A (pt) 2004-12-20 2005-12-12 dispositivo para emitir um sinal de autorização, sistema para controlar pelo menos um motor de aeronave e aeronave

Country Status (11)

Country Link
US (1) US7856295B2 (pt)
EP (1) EP1827978B1 (pt)
JP (1) JP4854674B2 (pt)
CN (1) CN100484835C (pt)
AT (1) ATE415343T1 (pt)
BR (1) BRPI0517110A (pt)
CA (1) CA2586885C (pt)
DE (1) DE602005011332D1 (pt)
FR (1) FR2879562B1 (pt)
RU (1) RU2353549C1 (pt)
WO (1) WO2006067295A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2934065B1 (fr) * 2008-07-17 2010-08-27 Airbus France Dispositif pour la determination de la position d'une manette des gaz dans un aeronef
FR2946018B1 (fr) * 2009-06-02 2012-09-28 Airbus France Dispositif pour compenser la perte de poussee d'un moteur d'aeronef et systeme de communication entre lesdits moteurs et un calculateur comportant ledit dispositif.
FR2956380B1 (fr) 2010-02-15 2012-07-13 Snecma Procede et dispositif de protection contre des anomalies de commande de poussee de moteur d'avion
KR101750773B1 (ko) 2016-01-20 2017-06-27 한국항공우주산업 주식회사 안전성이 향상된 장비 동작 제어 장치
CN110030093B (zh) * 2019-04-01 2021-05-25 中国航发沈阳发动机研究所 基于状态识别的舰载机发动机主燃油控制方法及装置
CN110030110B (zh) * 2019-04-01 2021-05-25 中国航发沈阳发动机研究所 基于状态识别的舰载机发动机气动稳定性提升方法及装置
FR3094807B1 (fr) 2019-04-05 2021-03-12 Safran Aircraft Engines Dispositif de commande d'un moteur d'un aéronef comprenant deux voies de commande redondées
US11306664B2 (en) * 2020-04-10 2022-04-19 Gulfstream Aerospace Corporation System and method to prevent unintended aircraft engine shutdown
FR3145345A1 (fr) * 2023-01-30 2024-08-02 Airbus Operations Dispositif d’inhibition d’une coupure d’un moteur de propulsion pour aeronef
JP7794147B2 (ja) * 2023-02-28 2026-01-06 トヨタ自動車株式会社 車両制御装置

Family Cites Families (17)

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Publication number Priority date Publication date Assignee Title
GB528963A (en) * 1939-03-31 1940-11-12 Charles Richard Fairey Improvements in or relating to safety devices for aircraft
US2938683A (en) * 1955-06-06 1960-05-31 Boeing Co Power control mechanism for jet powered aircraft
US3801372A (en) * 1971-08-18 1974-04-02 United Aircraft Corp Fuel cell system comprising separate coolant loop and sensing means
US5106035A (en) * 1989-12-29 1992-04-21 Aurora Flight Sciences Corporation Aircraft propulsion system using air liquefaction and storage
DE4119334A1 (de) * 1991-06-12 1992-12-17 Sen Rolf Herzog Anti-umkehrstroemungs-sicherungsgeraet fuer flugzeuge
US5285634A (en) * 1991-12-09 1994-02-15 United Technologies Corporation Aircraft gas turbine engine control
US5810284A (en) * 1995-03-15 1998-09-22 Hibbs; Bart D. Aircraft
US6119979A (en) * 1997-09-15 2000-09-19 Sky Station International, Inc. Cyclical thermal management system
JP4464474B2 (ja) * 1998-06-25 2010-05-19 トヨタ自動車株式会社 燃料電池システム、燃料電池車両及び燃料電池制御方法
US6322915B1 (en) * 1999-07-20 2001-11-27 International Fuel Cells Llc Humidification system for a fuel cell power plant
BR0110056A (pt) * 2000-04-03 2003-12-30 Aerovironment Inc Aeronave estratosférica movida a hidrogênio lìquido, sua asa, sistema de energia e método para o fornecimento de um reagente gasoso a uma célula de combustìvel numa taxa de fluxo de funcionamento desejada
DE60132896T2 (de) * 2000-07-24 2009-02-12 Honeywell International Inc. Detektion eines flugzeugstarts mit geringer leistung zum verwenden in einem bodennäherungswarnsystem
US6568633B2 (en) * 2000-08-24 2003-05-27 James P. Dunn Fuel cell powered electric aircraft
US20030230671A1 (en) * 2000-08-24 2003-12-18 Dunn James P. Fuel cell powered electric aircraft
DE60235317D1 (de) * 2001-11-13 2010-03-25 Goodrich Pump & Engine Control Fehlerverwaltungssystem für gasturbinentriebwerke
US20040088085A1 (en) * 2002-10-30 2004-05-06 Pratt & Whitney Canada Corp. Method and system for preventing un-commanded power surge of aircraft engine
FR2859176B1 (fr) * 2003-09-03 2005-10-28 Airbus France Aeronef pourvu d'inverseurs de poussee

Also Published As

Publication number Publication date
DE602005011332D1 (de) 2009-01-08
WO2006067295A1 (fr) 2006-06-29
FR2879562B1 (fr) 2008-05-16
JP4854674B2 (ja) 2012-01-18
EP1827978A1 (fr) 2007-09-05
RU2007127709A (ru) 2009-01-27
JP2008524059A (ja) 2008-07-10
US7856295B2 (en) 2010-12-21
US20090240386A1 (en) 2009-09-24
CA2586885A1 (fr) 2006-06-29
CA2586885C (fr) 2012-10-16
ATE415343T1 (de) 2008-12-15
FR2879562A1 (fr) 2006-06-23
RU2353549C1 (ru) 2009-04-27
CN101084148A (zh) 2007-12-05
EP1827978B1 (fr) 2008-11-26
CN100484835C (zh) 2009-05-06

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 11A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]