CA2787579C - Method and system for integrating engine control and flight control system - Google Patents

Method and system for integrating engine control and flight control system Download PDF

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Publication number
CA2787579C
CA2787579C CA2787579A CA2787579A CA2787579C CA 2787579 C CA2787579 C CA 2787579C CA 2787579 A CA2787579 A CA 2787579A CA 2787579 A CA2787579 A CA 2787579A CA 2787579 C CA2787579 C CA 2787579C
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CA
Canada
Prior art keywords
control system
engine
flight control
flight
information
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
CA2787579A
Other languages
English (en)
French (fr)
Other versions
CA2787579A1 (en
Inventor
Harry Kirk Mathews, Jr
Sridhar Adibhatla
Jeffrey Russell Bult
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to CA3065735A priority Critical patent/CA3065735A1/en
Publication of CA2787579A1 publication Critical patent/CA2787579A1/en
Application granted granted Critical
Publication of CA2787579C publication Critical patent/CA2787579C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • 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
    • 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
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/18502—Airborne stations
    • H04B7/18506—Communications with or from aircraft, i.e. aeronautical mobile service
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Signal Processing (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • Traffic Control Systems (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Feedback Control In General (AREA)
  • Navigation (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
CA2787579A 2011-08-30 2012-08-23 Method and system for integrating engine control and flight control system Expired - Fee Related CA2787579C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA3065735A CA3065735A1 (en) 2011-08-30 2012-08-23 Method and system for integrating engine control and flight control system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/221,102 2011-08-30
US13/221,102 US8634972B2 (en) 2011-08-30 2011-08-30 Method and system for integrating engine control and flight control system

Related Child Applications (1)

Application Number Title Priority Date Filing Date
CA3065735A Division CA3065735A1 (en) 2011-08-30 2012-08-23 Method and system for integrating engine control and flight control system

Publications (2)

Publication Number Publication Date
CA2787579A1 CA2787579A1 (en) 2013-02-28
CA2787579C true CA2787579C (en) 2020-03-10

Family

ID=47215356

Family Applications (2)

Application Number Title Priority Date Filing Date
CA2787579A Expired - Fee Related CA2787579C (en) 2011-08-30 2012-08-23 Method and system for integrating engine control and flight control system
CA3065735A Abandoned CA3065735A1 (en) 2011-08-30 2012-08-23 Method and system for integrating engine control and flight control system

Family Applications After (1)

Application Number Title Priority Date Filing Date
CA3065735A Abandoned CA3065735A1 (en) 2011-08-30 2012-08-23 Method and system for integrating engine control and flight control system

Country Status (6)

Country Link
US (2) US8634972B2 (enExample)
EP (1) EP2565425B1 (enExample)
JP (1) JP2013049412A (enExample)
CN (2) CN106314764B (enExample)
BR (1) BR102012020961A2 (enExample)
CA (2) CA2787579C (enExample)

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US9758252B2 (en) 2012-08-23 2017-09-12 General Electric Company Method, system, and apparatus for reducing a turbine clearance
US10184348B2 (en) 2013-12-05 2019-01-22 Honeywell International Inc. System and method for turbine blade clearance control
EP2887015A1 (en) * 2013-12-18 2015-06-24 The Boeing Company Assessing feasability of an aircraft trajectory
US10347140B2 (en) 2014-03-11 2019-07-09 Textron Innovations Inc. Flight planning and communication
WO2015138327A1 (en) 2014-03-11 2015-09-17 Cessna Aircraft Company Touch screen instrument panel
US9260188B1 (en) * 2014-08-18 2016-02-16 Gulfstream Aerospace Corporation Apparatus and method for allowing multi-mode use of an aircraft cockpit
CN105739453A (zh) * 2014-12-10 2016-07-06 西安航空动力控制科技有限公司 一种基于分布式控制理念的智能进口导叶控制方法及装置
US9607452B2 (en) 2015-04-21 2017-03-28 United Technologies Corporation Electronic module integration for harsh environment machines
CN104890889B (zh) * 2015-05-13 2017-02-22 深圳一电航空技术有限公司 飞行器控制方法及飞行器
CN104898694B (zh) * 2015-05-13 2019-02-19 深圳一电航空技术有限公司 飞行器控制方法及飞行器
US10035609B2 (en) 2016-03-08 2018-07-31 Harris Corporation Wireless engine monitoring system for environmental emission control and aircraft networking
US9828108B2 (en) * 2016-03-10 2017-11-28 The Boeing Company Automated flight throttle control
US10260883B2 (en) 2016-06-29 2019-04-16 General Electric Company Methods and systems for optimal guidance based on energy state approximation
CN106586002B (zh) * 2016-11-30 2018-12-11 中国航空工业集团公司沈阳飞机设计研究所 一种飞机与发动机一体化匹配调节控制方法
CN107512400B (zh) * 2017-09-04 2020-12-15 江西洪都航空工业集团有限责任公司 串列双座飞机全权限数字控制装置分布式安装结构
US11203440B2 (en) 2018-01-04 2021-12-21 Hamilton Sundstrand Corporation System for integrated engine and flight control
US10746042B2 (en) 2018-03-23 2020-08-18 Raytheon Technologyies Corporation Systems and methods for active clearance control based on selected operating mode
CN108945397B (zh) * 2018-04-24 2021-05-04 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种飞行驾驶系统
FR3098845B1 (fr) * 2019-07-19 2021-12-24 Safran Aircraft Engines Procédé de commande d’une vanne de pilotage de jeux lors d’une montée étagée en phase de croisière
US11956063B2 (en) * 2019-11-14 2024-04-09 General Electric Company Engine control system
CN112855346B (zh) * 2019-11-27 2022-06-17 中国航发商用航空发动机有限责任公司 推力控制方法、系统及航空发动机
US11692494B2 (en) 2021-02-10 2023-07-04 Honeywell International Inc. Automated engine vibration monitoring and control system

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US6259976B1 (en) 1999-09-25 2001-07-10 Jerome H. Lemelson Fuzzy logic based emergency flight control with thrust vectoring
US6894611B2 (en) * 2002-09-23 2005-05-17 General Electric Company Method and system for uploading and downloading engine control data
FR2854964B1 (fr) * 2003-05-16 2007-08-03 Thales Sa Systeme de protection automatique du vol pour aeronef
CN100444138C (zh) * 2003-07-23 2008-12-17 哈里公司 无线发动机监控系统
US7620374B2 (en) * 2004-09-16 2009-11-17 Harris Corporation System and method of transmitting data from an aircraft
US7437225B1 (en) * 2005-07-29 2008-10-14 Rockwell Collins, Inc. Flight management system
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Also Published As

Publication number Publication date
CN106314764A (zh) 2017-01-11
EP2565425A3 (en) 2017-05-17
US8634972B2 (en) 2014-01-21
CA3065735A1 (en) 2013-02-28
CN102963523A (zh) 2013-03-13
US20140136030A1 (en) 2014-05-15
JP2013049412A (ja) 2013-03-14
CN106314764B (zh) 2019-05-14
CN102963523B (zh) 2016-12-21
CA2787579A1 (en) 2013-02-28
BR102012020961A2 (pt) 2013-11-12
US20130054055A1 (en) 2013-02-28
US9145202B2 (en) 2015-09-29
EP2565425B1 (en) 2020-09-30
EP2565425A2 (en) 2013-03-06

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Effective date: 20170621

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