JPS5059612A - - Google Patents

Info

Publication number
JPS5059612A
JPS5059612A JP49107903A JP10790374A JPS5059612A JP S5059612 A JPS5059612 A JP S5059612A JP 49107903 A JP49107903 A JP 49107903A JP 10790374 A JP10790374 A JP 10790374A JP S5059612 A JPS5059612 A JP S5059612A
Authority
JP
Japan
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.)
Pending
Application number
JP49107903A
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 filed Critical
Publication of JPS5059612A publication Critical patent/JPS5059612A/ja
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F11/00Error detection; Error correction; Monitoring
    • G06F11/07Responding to the occurrence of a fault, e.g. fault tolerance
    • G06F11/16Error detection or correction of the data by redundancy in hardware
    • G06F11/1629Error detection by comparing the output of redundant processing systems
    • G06F11/165Error detection by comparing the output of redundant processing systems with continued operation after detection of the error
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02Initiating means
    • B64D31/06Initiating means actuated automatically
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B9/00Safety arrangements
    • G05B9/02Safety arrangements electric
    • G05B9/03Safety arrangements electric with multiple-channel loop, i.e. redundant control systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Quality & Reliability (AREA)
  • General Engineering & Computer Science (AREA)
  • Safety Devices In Control Systems (AREA)
  • Testing And Monitoring For Control Systems (AREA)
  • Control By Computers (AREA)
JP49107903A 1973-09-24 1974-09-20 Pending JPS5059612A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4463673 1973-09-24

Publications (1)

Publication Number Publication Date
JPS5059612A true JPS5059612A (ja) 1975-05-23

Family

ID=10434157

Family Applications (1)

Application Number Title Priority Date Filing Date
JP49107903A Pending JPS5059612A (ja) 1973-09-24 1974-09-20

Country Status (7)

Country Link
US (1) US4032757A (ja)
JP (1) JPS5059612A (ja)
CA (1) CA1026850A (ja)
DE (1) DE2445173A1 (ja)
FR (1) FR2245020B1 (ja)
IT (1) IT1021662B (ja)
SE (1) SE403085B (ja)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03278101A (ja) * 1990-03-28 1991-12-09 Nissan Motor Co Ltd 信号処理装置
JPH0573238U (ja) * 1991-09-25 1993-10-08 株式会社三陽電機製作所 エンジン制御装置
JP2006316773A (ja) * 2005-05-16 2006-11-24 Honda Motor Co Ltd 航空機用ガスタービン・エンジンの制御装置
WO2007135991A1 (ja) * 2006-05-19 2007-11-29 Ihi Corporation ストール予兆検知装置及び方法、並びにエンジン制御システム
US20110046863A1 (en) * 2009-08-24 2011-02-24 Honda Motor Co., Ltd. Control apparatus for aeroplane gas turbine engine
CN102865147A (zh) * 2011-07-06 2013-01-09 中国航空工业集团公司沈阳发动机设计研究所 一种采用双余度控制规律处理控制传感器信号故障的方法

Families Citing this family (74)

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JPS5831602B2 (ja) * 1976-02-04 1983-07-07 株式会社日立製作所 二重系制御装置
FR2344063A1 (fr) * 1976-03-10 1977-10-07 Smiths Industries Ltd Circuit numerique de commande a deux voies au moins
US4136517A (en) * 1976-07-06 1979-01-30 General Electric Company Thrust control system for a gas turbine engine
US4228496A (en) * 1976-09-07 1980-10-14 Tandem Computers Incorporated Multiprocessor system
DE2734542A1 (de) * 1976-09-09 1978-03-23 Gen Electric Regelanordnung und verfahren zur automatischen eichung des nullfehlers der temperatur-regelparameter einer gasturbine
DE2701924C3 (de) * 1977-01-19 1987-07-30 Standard Elektrik Lorenz Ag, 7000 Stuttgart Steuereinrichtung für spurgebundene Fahrzeuge
CA1118101A (en) * 1977-06-02 1982-02-09 Jerry Doniger Digital flight guidance system
GB1587792A (en) * 1977-06-02 1981-04-08 Bendix Corp Digital flight guidance system
US4096989A (en) * 1977-06-20 1978-06-27 The Bendix Corporation Monitoring apparatus for redundant control systems
US4154395A (en) * 1977-11-25 1979-05-15 General Electric Company Redundant signal circuit
FR2430633A1 (fr) * 1978-07-07 1980-02-01 Sfena Systeme de commande auto-surveille, d'un processus
US4215412A (en) * 1978-07-13 1980-07-29 The Boeing Company Real time performance monitoring of gas turbine engines
US4270168A (en) * 1978-08-31 1981-05-26 United Technologies Corporation Selective disablement in fail-operational, fail-safe multi-computer control system
US4268354A (en) * 1978-10-12 1981-05-19 Westinghouse Electric Corp. Nuclear reactor in core flux mapping system
US4313167A (en) * 1979-07-27 1982-01-26 General Electric Company Thrust control system for a gas turbine engine
US4387426A (en) * 1979-09-06 1983-06-07 Rolls-Royce Limited Digital data processing system
US4302821A (en) * 1979-10-30 1981-11-24 Pitney-Bowes, Inc. Interposer control for electronic postage meter
US4444048A (en) * 1979-11-10 1984-04-24 Robert Bosch Gmbh Apparatus for detecting malfunction in cyclically repetitive processes in an internal combustion engine
US4313201A (en) * 1980-03-05 1982-01-26 United Technologies Corporation Tested, dissimilar helicopter stability augmentation
US4377000A (en) * 1980-05-05 1983-03-15 Westinghouse Electric Corp. Automatic fault detection and recovery system which provides stability and continuity of operation in an industrial multiprocessor control
JPS5717019A (en) * 1980-07-07 1982-01-28 Fanuc Ltd Numerical controller
US4370706A (en) * 1980-09-26 1983-01-25 The Bendix Corporation Controller for a dual servo system
US4410948A (en) * 1981-02-13 1983-10-18 The Bendix Corporation Multi-engine autothrottle providing automatic engine EPR equalization
US4504905A (en) * 1981-09-05 1985-03-12 Lucas Industries Plc Digital control system including means for maintaining signals supplied thereby within limiting values
FR2512980B1 (ja) * 1981-09-14 1983-12-23 Aero Etudes Conseils
EP0110885B1 (en) * 1982-06-16 1989-09-06 The Boeing Company Autopilot flight director system
US4541094A (en) * 1983-03-21 1985-09-10 Sequoia Systems, Inc. Self-checking computer circuitry
GB8312822D0 (en) * 1983-05-10 1983-06-15 Dowty & Smiths Ind Controls Lt Engine control systems
US4634110A (en) * 1983-07-28 1987-01-06 Harris Corporation Fault detection and redundancy management system
US4599695A (en) * 1984-05-25 1986-07-08 Motorola, Inc. Microprocessor transient interrupt system adaptable for engine control
US4622667A (en) * 1984-11-27 1986-11-11 Sperry Corporation Digital fail operational automatic flight control system utilizing redundant dissimilar data processing
US4722061A (en) * 1984-12-20 1988-01-26 United Technologies Corporation Establishing synthesis validity between two signal sources
US4799159A (en) * 1985-05-30 1989-01-17 Honeywell Inc. Digital automatic flight control system with disparate function monitoring
US4656634A (en) * 1985-06-14 1987-04-07 Motorola, Inc. Skew insensitive fault detect and signal routing device
US4787041A (en) * 1985-08-01 1988-11-22 Honeywell Data control system for digital automatic flight control system channel with plural dissimilar data processing
US4821193A (en) * 1985-08-26 1989-04-11 General Electric Company Digital control for gas turbine engine
FR2591777B1 (fr) * 1985-12-13 1991-03-15 Cimsa Sintra Reseau informatise de grande securite de fonctionnement et procede de commande utilisant un tel reseau
US4662171A (en) * 1986-03-31 1987-05-05 The Boeing Company Automatic thrust restoration system
US4785403A (en) * 1986-05-02 1988-11-15 United Technologies Corporation Distributed flight condition data validation system and method
JPS62299435A (ja) * 1986-06-19 1987-12-26 Isuzu Motors Ltd 異常検出装置付き車両の制御装置
DE3638947C2 (de) * 1986-11-14 1995-08-31 Bosch Gmbh Robert Verfahren zur Synchronisation von Rechnern eines Mehrrechnersystems und Mehrrechnersystem
JPS63133202A (ja) * 1986-11-25 1988-06-06 Mitsubishi Electric Corp 車両用制御装置
US4918629A (en) * 1988-04-07 1990-04-17 The Boeing Company Engine trim tachometer unit and calibration method
DE3825280A1 (de) * 1988-07-26 1990-02-01 Bayerische Motoren Werke Ag Steuersystem fuer stelleinrichtungen eines kraftfahrzeugs
FR2643502B1 (fr) * 1989-02-20 1996-01-19 Aerospatiale Dispositif de commande a manche basculant, notamment pour aeronef, et systeme comportant un tel dispositif
US5001638A (en) * 1989-04-18 1991-03-19 The Boeing Company Integrated aircraft air data system
US5086499A (en) * 1989-05-23 1992-02-04 Aeg Westinghouse Transportation Systems, Inc. Computer network for real time control with automatic fault identification and by-pass
US5043911A (en) * 1989-12-22 1991-08-27 Sundstrand Corporation Multiplexing A/D converter for a generator control unit
FR2670592A1 (fr) * 1990-12-14 1992-06-19 Sextant Avionique Procede et systeme de securisation des informations de pilotage d'un aeronef.
US5274554A (en) * 1991-02-01 1993-12-28 The Boeing Company Multiple-voting fault detection system for flight critical actuation control systems
US5206810A (en) * 1991-02-07 1993-04-27 General Electric Company Redundant actuator control
FR2680386B1 (fr) * 1991-08-12 1993-11-05 Aerospatiale Ste Nationale Indle Dispositif pour la commande du regime des moteurs d'un aeronef.
DE4136338A1 (de) * 1991-11-05 1993-05-06 Robert Bosch Gmbh, 7000 Stuttgart, De Verfahren und vorrichtung zur fehlerbehandlung in elektronischen steuergeraeten
US5428769A (en) * 1992-03-31 1995-06-27 The Dow Chemical Company Process control interface system having triply redundant remote field units
US5279107A (en) * 1992-06-30 1994-01-18 United Technologies Corporation Fuel control system with fuel metering valve fault accommodation
FR2710026B1 (fr) * 1993-09-17 1995-12-08 Aerospatiale Dispositif de surveillance du système propulsif d'un aéronef.
US5436826A (en) * 1993-10-20 1995-07-25 United Technologies Corporation Dual control with dual sensor averaging and substitution
US5949677A (en) * 1997-01-09 1999-09-07 Honeywell Inc. Control system utilizing fault detection
EP1298503A1 (de) * 2001-09-28 2003-04-02 Claus Haag Joystick-Steuerung
JP4490963B2 (ja) 2003-02-15 2010-06-30 ガルフストリーム・エアロスペース・コーポレイション 航空機キャビン大気組成制御方法
US7043896B2 (en) * 2003-11-21 2006-05-16 Pratt & Whitney Canada Corp. Method and apparatus for controlling fuel flow to an engine
US7509810B2 (en) * 2004-11-10 2009-03-31 Honeywell International Inc. Inter-turbine temperature display compensation method
EP1977297A4 (en) * 2006-01-17 2010-02-24 Gulfstream Aerospace Corp APPARATUS AND METHOD FOR CONTROLLING RELIEF USED IN DISTRIBUTED FLIGHT CONTROL SYSTEM
WO2007084529A2 (en) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation System and method for an integrated backup control system
GB0624090D0 (en) * 2006-12-01 2007-01-10 Selamine Ltd Ramipril amine salts
US8036805B2 (en) * 2007-07-13 2011-10-11 Honeywell International Inc. Distributed engine control system
US8948960B2 (en) * 2007-11-30 2015-02-03 Honeywell International Inc. Systems and methods for arbitrating sensor and actuator signals in a multi-channel control system
US8370046B2 (en) * 2010-02-11 2013-02-05 General Electric Company System and method for monitoring a gas turbine
US8775052B2 (en) * 2011-12-15 2014-07-08 GM Global Technology Operations LLC Sensors bias detection for electronic returnless fuel system
FR2989735B1 (fr) 2012-04-19 2015-12-11 Snecma Procede de gestion du fonctionnement d'un dispositif de dosage d'un systeme d'injection de carburant de turbomachine
FR2990002B1 (fr) * 2012-04-27 2016-01-22 Snecma Turbomachine comportant un systeme de surveillance comprenant un module d'engagement d'une fonction de protection de la turbomachine et procede de surveillance
FR3023872B1 (fr) * 2014-07-21 2016-07-15 Sagem Defense Securite Dispositif de protection contre survitesse d'un moteur d'aeronef
CN111058958B (zh) * 2019-12-11 2022-01-07 厦门林巴贺航空发动机股份有限公司 一种活塞式航空发动机的控制方法
CN113946122B (zh) * 2021-10-22 2024-02-13 中国科学院工程热物理研究所 一种基于置信度权值浮动的燃气轮机参数多余度表决方法

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4861886A (ja) * 1971-12-02 1973-08-29

Family Cites Families (7)

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US3143693A (en) * 1960-02-26 1964-08-04 Smiths America Corp Automatic trimming systems for the control surfaces of a moving craft
DE1524239B2 (de) * 1965-11-16 1971-07-22 Telefonaktiebolaget Lm Ericsson, Stockholm Schaltungsanordnung zur aufrechterhaltung eines fehler freien betriebes bei einer rechenanlage mit mindestens zwei parallel arbeitenden rechengeraeten
US3476922A (en) * 1966-08-05 1969-11-04 Sperry Rand Corp Failure monitor for redundant channel systems
US3679956A (en) * 1970-02-02 1972-07-25 Ltv Electrosystems Inc Multiple servomotor actuator
US3688099A (en) * 1971-04-28 1972-08-29 Lear Siegler Inc Automatic control system with a digital computer
FR2162093B1 (ja) * 1971-12-02 1977-04-08 Hitachi Ltd
US3834361A (en) * 1972-08-23 1974-09-10 Bendix Corp Back-up fuel control system

Patent Citations (1)

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Publication number Priority date Publication date Assignee Title
JPS4861886A (ja) * 1971-12-02 1973-08-29

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03278101A (ja) * 1990-03-28 1991-12-09 Nissan Motor Co Ltd 信号処理装置
JPH0573238U (ja) * 1991-09-25 1993-10-08 株式会社三陽電機製作所 エンジン制御装置
JP2006316773A (ja) * 2005-05-16 2006-11-24 Honda Motor Co Ltd 航空機用ガスタービン・エンジンの制御装置
US7840336B2 (en) 2005-05-16 2010-11-23 Honda Motor Co., Ltd. Control system for gas turbine aeroengine
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
WO2007135991A1 (ja) * 2006-05-19 2007-11-29 Ihi Corporation ストール予兆検知装置及び方法、並びにエンジン制御システム
US8185291B2 (en) 2006-05-19 2012-05-22 Ihi Corporation Stall prediction apparatus, prediction method thereof, and engine control system
US20110046863A1 (en) * 2009-08-24 2011-02-24 Honda Motor Co., Ltd. Control apparatus for aeroplane gas turbine engine
JP2011043135A (ja) * 2009-08-24 2011-03-03 Honda Motor Co Ltd 航空機用ガスタービン・エンジンの制御装置
US9556800B2 (en) 2009-08-24 2017-01-31 Honda Motor Co., Ltd. Control apparatus for aeroplane gas turbine engine
CN102865147A (zh) * 2011-07-06 2013-01-09 中国航空工业集团公司沈阳发动机设计研究所 一种采用双余度控制规律处理控制传感器信号故障的方法

Also Published As

Publication number Publication date
DE2445173A1 (de) 1975-03-27
SE7411916L (ja) 1975-03-25
IT1021662B (it) 1978-02-20
FR2245020B1 (ja) 1978-06-09
US4032757A (en) 1977-06-28
FR2245020A1 (ja) 1975-04-18
CA1026850A (en) 1978-02-21
SE403085B (sv) 1978-07-31

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