CN101808900B - 在fadec和航空电子组件之间分配的结构 - Google Patents

在fadec和航空电子组件之间分配的结构 Download PDF

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Publication number
CN101808900B
CN101808900B CN200880105443.XA CN200880105443A CN101808900B CN 101808900 B CN101808900 B CN 101808900B CN 200880105443 A CN200880105443 A CN 200880105443A CN 101808900 B CN101808900 B CN 101808900B
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engine
avionics
aircraft
data
interface
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Chinese (zh)
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CN101808900A (zh
Inventor
L·圣马克
L·布吕内尔
P·扎卡里亚
M·亚历山大
J·费奥
F·勒博尔纳
T·伊莫尔迪诺
J-F·贝尔卡迪
N·迪朗
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Airbus Operations SAS
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Airbus Operations SAS
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Retarders (AREA)
CN200880105443.XA 2007-09-03 2008-08-20 在fadec和航空电子组件之间分配的结构 Active CN101808900B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0757333 2007-09-03
FR0757333A FR2920410B1 (fr) 2007-09-03 2007-09-03 Architecture repartie entre un fadec et des composants avioniques
PCT/FR2008/051512 WO2009030856A2 (fr) 2007-09-03 2008-08-20 Architecture repartie entre un fadec et des composants avioniques

Publications (2)

Publication Number Publication Date
CN101808900A CN101808900A (zh) 2010-08-18
CN101808900B true CN101808900B (zh) 2015-11-25

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ID=39284247

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CN200880105443.XA Active CN101808900B (zh) 2007-09-03 2008-08-20 在fadec和航空电子组件之间分配的结构

Country Status (9)

Country Link
US (1) US8825227B2 (enExample)
EP (1) EP2195240B1 (enExample)
JP (1) JP5416114B2 (enExample)
CN (1) CN101808900B (enExample)
BR (1) BRPI0817179A2 (enExample)
CA (1) CA2698106C (enExample)
FR (1) FR2920410B1 (enExample)
RU (1) RU2483005C2 (enExample)
WO (1) WO2009030856A2 (enExample)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2943036B1 (fr) * 2009-03-11 2011-04-15 Airbus France Systeme distribue de commande de vol implemente selon une architecture avionique modulaire integree.
US8295995B2 (en) * 2009-04-22 2012-10-23 Hamilton Sundstrand Corporation Distributed approach to electronic engine control for gas turbine engines
FR2946165B1 (fr) * 2009-06-02 2016-06-10 Airbus France Systeme de gestion automatique de controle de moteurs d'un aeronef.
FR2956163B1 (fr) * 2010-02-10 2012-02-17 Aircelle Sa Systeme de commande d'un aeronef
US8290683B2 (en) * 2010-02-16 2012-10-16 Telectro-Mek, Inc. Apparatus and method for reducing aircraft fuel consumption
US20120095662A1 (en) * 2010-10-14 2012-04-19 Hamilton Sundstrand Corporation Electronic engine control software reconfiguration for distributed eec operation
US9388744B2 (en) * 2012-03-30 2016-07-12 General Electric Company Distributed gas turbine engine control system with remote interface units
US9179570B2 (en) * 2012-07-31 2015-11-03 Simmonds Precision Products, Inc. Multi connector interconnect system
GB201303527D0 (en) * 2013-02-28 2013-04-10 Airbus Uk Ltd Aircraft inerting system
CA2905233C (en) 2013-03-14 2022-04-26 Rolls-Royce Corporation Intelligent integrated control system and method
EP2851291B1 (fr) * 2013-09-23 2016-05-11 Airbus Operations (S.A.S) Système de commande d'un aéronef
US9481471B2 (en) * 2013-11-11 2016-11-01 The Boeing Company Autonomous propulsion apparatus and methods
US10587307B2 (en) 2016-06-20 2020-03-10 Ge Aviation Systems, Llc Transmission of power and communication of signals over fuel and hydraulic lines in a vehicle
US10454525B2 (en) * 2016-06-20 2019-10-22 Ge Aviation Systems Llc Communication of signals over fuel lines in a vehicle
FR3065443B1 (fr) * 2017-04-19 2021-01-01 Airbus Group Sas Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee
US10044175B1 (en) * 2017-07-31 2018-08-07 Honeywell International Inc. High temperature avionic line replaceable units and aircraft systems containing the same
US11203440B2 (en) 2018-01-04 2021-12-21 Hamilton Sundstrand Corporation System for integrated engine and flight control
US10906634B2 (en) 2018-01-22 2021-02-02 Hamilton Sunstrand Corporation Electric vehicle management architecture
US11391218B2 (en) * 2019-03-22 2022-07-19 Pratt & Whitney Canada Corp. Method and system for setting power of an aircraft engine
US11561873B2 (en) 2019-09-26 2023-01-24 General Electric Company Test equipment interface add-on having a production support equipment module and a selectively removable test support equipment module
EP3799349B1 (en) 2019-09-26 2023-11-08 General Electric Company Communicating securely with devices in a distributed control system
US12459659B2 (en) 2022-03-07 2025-11-04 General Electric Company Method and apparatus for controlling electrical machines operating with a turbine engine
US12006880B2 (en) 2022-09-12 2024-06-11 General Electric Company High bandwidth control of turbofan/turboprop thrust response using embedded electric machines
US12284272B2 (en) 2022-09-30 2025-04-22 General Electric Company Methods and systems for starting secure communication in systems with high availability

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5270931A (en) * 1989-02-23 1993-12-14 The Boeing Company Software controlled aircraft component configuration system
WO1996041260A1 (en) * 1995-06-07 1996-12-19 Alliedsignal Inc. Reconfigurable algorithmic networks for aircraft data management
CN1172208A (zh) * 1996-05-15 1998-02-04 波音公司 给航电系统自动提供喷气发动机推力额定值的方法和装置
GB2427711A (en) * 2005-05-16 2007-01-03 Honda Motor Co Ltd Control system for gas turbine aeroengine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5136841A (en) * 1989-02-27 1992-08-11 Zimmerman Ward H Aircraft propulsion control system
US6443399B1 (en) * 2000-07-14 2002-09-03 Honeywell International Inc. Flight control module merged into the integrated modular avionics
US20050027826A1 (en) * 2001-12-03 2005-02-03 Loda David C. Microserver test port retrofit kit
RU30708U1 (ru) * 2003-02-10 2003-07-10 Федеральное государственное унитарное предприятие Лётно-исследовательский институт им. М.М.Громова Сетевая система контроля работы самолётных силовых установок
US7406370B2 (en) * 2004-08-24 2008-07-29 Honeywell International Inc. Electrical energy management system on a more electric vehicle
RU49297U1 (ru) * 2005-07-06 2005-11-10 Федеральное государственное унитарное предприятие Научно-исследовательский институт авиационного оборудования Информационно-управляющий комплекс летательных аппаратов
DE102005055000A1 (de) * 2005-11-18 2007-05-24 Airbus Deutschland Gmbh Modulares Avioniksystem eines Flugzeuges
US8036805B2 (en) * 2007-07-13 2011-10-11 Honeywell International Inc. Distributed engine control system
US8306421B1 (en) * 2008-05-05 2012-11-06 Rockwell Collins, Inc. Passive optical avionics network including optical repeater
US8078055B1 (en) * 2008-05-05 2011-12-13 Rockwell Collins, Inc. Passive optical avionics network
US8391788B1 (en) * 2009-02-20 2013-03-05 Rockwell Collins, Inc. Remote concentration system for an integrated modular avionics system
US8301867B1 (en) * 2009-08-10 2012-10-30 Rockwell Collins, Inc. Secondary core ONU to OLT via internal EPON bus coupled multi-core processor for integrated modular avionic system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5270931A (en) * 1989-02-23 1993-12-14 The Boeing Company Software controlled aircraft component configuration system
WO1996041260A1 (en) * 1995-06-07 1996-12-19 Alliedsignal Inc. Reconfigurable algorithmic networks for aircraft data management
CN1172208A (zh) * 1996-05-15 1998-02-04 波音公司 给航电系统自动提供喷气发动机推力额定值的方法和装置
GB2427711A (en) * 2005-05-16 2007-01-03 Honda Motor Co Ltd Control system for gas turbine aeroengine

Also Published As

Publication number Publication date
FR2920410A1 (fr) 2009-03-06
JP5416114B2 (ja) 2014-02-12
EP2195240B1 (fr) 2012-06-27
CA2698106C (en) 2016-08-02
JP2010537872A (ja) 2010-12-09
FR2920410B1 (fr) 2009-10-30
CN101808900A (zh) 2010-08-18
RU2483005C2 (ru) 2013-05-27
US20100292870A1 (en) 2010-11-18
BRPI0817179A2 (pt) 2015-03-17
WO2009030856A3 (fr) 2009-04-30
RU2010112849A (ru) 2011-10-10
EP2195240A2 (fr) 2010-06-16
WO2009030856A2 (fr) 2009-03-12
CA2698106A1 (en) 2009-03-12
US8825227B2 (en) 2014-09-02

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