JP2010537872A5 - - Google Patents

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Publication number
JP2010537872A5
JP2010537872A5 JP2010522420A JP2010522420A JP2010537872A5 JP 2010537872 A5 JP2010537872 A5 JP 2010537872A5 JP 2010522420 A JP2010522420 A JP 2010522420A JP 2010522420 A JP2010522420 A JP 2010522420A JP 2010537872 A5 JP2010537872 A5 JP 2010537872A5
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JP
Japan
Prior art keywords
engine
aircraft
interface
control device
engine interface
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.)
Granted
Application number
JP2010522420A
Other languages
English (en)
Japanese (ja)
Other versions
JP5416114B2 (ja
JP2010537872A (ja
Filing date
Publication date
Priority claimed from FR0757333A external-priority patent/FR2920410B1/fr
Application filed filed Critical
Publication of JP2010537872A publication Critical patent/JP2010537872A/ja
Publication of JP2010537872A5 publication Critical patent/JP2010537872A5/ja
Application granted granted Critical
Publication of JP5416114B2 publication Critical patent/JP5416114B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2010522420A 2007-09-03 2008-08-20 Ｆａｄｅｃとアビオニクス部品に分配されるアーキテクチャ Expired - Fee Related JP5416114B2 (ja)

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 (3)

Publication Number Publication Date
JP2010537872A JP2010537872A (ja) 2010-12-09
JP2010537872A5 true JP2010537872A5 (enExample) 2011-10-06
JP5416114B2 JP5416114B2 (ja) 2014-02-12

Family

ID=39284247

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010522420A Expired - Fee Related JP5416114B2 (ja) 2007-09-03 2008-08-20 Ｆａｄｅｃとアビオニクス部品に分配されるアーキテクチャ

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

Family Cites Families (16)

* 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
US5136841A (en) * 1989-02-27 1992-08-11 Zimmerman Ward H Aircraft propulsion control system
US5761625A (en) * 1995-06-07 1998-06-02 Alliedsignal Inc. Reconfigurable algorithmic networks for aircraft data management
US5893040A (en) * 1996-05-15 1999-04-06 The Boeing Company Method and apparatus for automatically providing jet engine thrust ratings to avionic systems
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
JP4657800B2 (ja) * 2005-05-16 2011-03-23 本田技研工業株式会社 航空機用ガスタービン・エンジンの制御装置
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

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