GB2095755A - Multiple gas turbine speed/temperature response control system - Google Patents

Multiple gas turbine speed/temperature response control system Download PDF

Info

Publication number
GB2095755A
GB2095755A GB8203816A GB8203816A GB2095755A GB 2095755 A GB2095755 A GB 2095755A GB 8203816 A GB8203816 A GB 8203816A GB 8203816 A GB8203816 A GB 8203816A GB 2095755 A GB2095755 A GB 2095755A
Authority
GB
United Kingdom
Prior art keywords
engine
power
temperature
turbine
pilot
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.)
Withdrawn
Application number
GB8203816A
Other languages
English (en)
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.)
Avco Corp
Original Assignee
Avco Corp
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 Avco Corp filed Critical Avco Corp
Publication of GB2095755A publication Critical patent/GB2095755A/en
Withdrawn legal-status Critical Current

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
    • F02C9/42—Control of fuel supply specially adapted for the control of two or more plants simultaneously
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control; Arrangement thereof
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • B64D31/12—Initiating means actuated automatically for equalising or synchronising power plants
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Turbines (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Controls For Constant Speed Travelling (AREA)
GB8203816A 1981-03-30 1982-02-10 Multiple gas turbine speed/temperature response control system Withdrawn GB2095755A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US24912581A 1981-03-30 1981-03-30

Publications (1)

Publication Number Publication Date
GB2095755A true GB2095755A (en) 1982-10-06

Family

ID=22942151

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8203816A Withdrawn GB2095755A (en) 1981-03-30 1982-02-10 Multiple gas turbine speed/temperature response control system

Country Status (8)

Country Link
JP (1) JPS57165632A (sv)
BR (1) BR8201832A (sv)
CA (1) CA1161527A (sv)
DE (1) DE3201010A1 (sv)
FR (1) FR2502697A1 (sv)
GB (1) GB2095755A (sv)
IT (1) IT1151860B (sv)
SE (1) SE8107800L (sv)

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0322343A2 (en) * 1987-12-22 1989-06-28 United Technologies Corporation Propeller phase control apparatus
EP0322342A2 (en) * 1987-12-22 1989-06-28 United Technologies Corporation Engine speed control apparatus
EP0369495A1 (en) * 1988-11-18 1990-05-23 The Boeing Company Automatic throttle controller for aircraft with intermixed engines
WO1994018045A1 (de) * 1993-02-08 1994-08-18 Witt & Sohn Gmbh & Co. Oberflächeneffektfahrzeug
EP1413762A2 (en) * 2002-10-23 2004-04-28 Honeywell Normalair-Garrett (Holdings) Limited A method of balancing the supply of bleed air from a plurality of gas turbine engines
WO2006059982A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Remote engine fuel control and electronic engine control for turbine engine
FR2902408A1 (fr) * 2006-06-19 2007-12-21 Eurocopter France Equilibrage en puissance de deux turbomoteurs d'un aeronef
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
US7854112B2 (en) 2004-12-01 2010-12-21 United Technologies Corporation Vectoring transition duct for turbine engine
US7882694B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Variable fan inlet guide vane assembly for gas turbine engine
US7921635B2 (en) 2004-12-01 2011-04-12 United Technologies Corporation Peripheral combustor for tip turbine engine
US7934902B2 (en) 2004-12-01 2011-05-03 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
US7937927B2 (en) 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
US7980054B2 (en) 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
US8024931B2 (en) 2004-12-01 2011-09-27 United Technologies Corporation Combustor for turbine engine
DE102010020024A1 (de) * 2010-05-10 2011-11-10 Rolls-Royce Deutschland Ltd & Co Kg Triebwerkssynchronisierverfahren
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US8561383B2 (en) 2004-12-01 2013-10-22 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
US8641367B2 (en) 2004-12-01 2014-02-04 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
GB2524775A (en) * 2014-04-02 2015-10-07 Rolls Royce Plc Aircraft vapour trail control system
US10801361B2 (en) 2016-09-09 2020-10-13 General Electric Company System and method for HPT disk over speed prevention

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4903086B2 (ja) * 2007-05-22 2012-03-21 トッパン・フォームズ株式会社 紙捌き装置
JP2009067586A (ja) * 2007-09-18 2009-04-02 Toppan Forms Co Ltd 紙捌き装置
FR3058278B1 (fr) * 2016-10-27 2020-02-28 Safran Electrical & Power Systeme pour l'alimentation d'actionneurs electriques embarques dans un aeronef

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US299630A (en) * 1884-06-03 Heistet eichling
GB724196A (en) * 1950-11-08 1955-02-16 Gen Motors Corp Improved control system for an aircraft power plant
US3174284A (en) * 1963-02-19 1965-03-23 United Aircraft Corp Power management fuel control for plural gas turbine engines
US4147035A (en) * 1978-02-16 1979-04-03 Semco Instruments, Inc. Engine load sharing control system

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0322343A2 (en) * 1987-12-22 1989-06-28 United Technologies Corporation Propeller phase control apparatus
EP0322342A2 (en) * 1987-12-22 1989-06-28 United Technologies Corporation Engine speed control apparatus
EP0322342A3 (en) * 1987-12-22 1989-10-18 United Technologies Corporation Engine speed control apparatus
EP0322343A3 (en) * 1987-12-22 1989-10-25 United Technologies Corporation Propeller phase control apparatus
EP0369495A1 (en) * 1988-11-18 1990-05-23 The Boeing Company Automatic throttle controller for aircraft with intermixed engines
WO1994018045A1 (de) * 1993-02-08 1994-08-18 Witt & Sohn Gmbh & Co. Oberflächeneffektfahrzeug
US5655616A (en) * 1993-02-08 1997-08-12 Witt; Hans Hovercraft and process of regulating air cushion
EP1413762A2 (en) * 2002-10-23 2004-04-28 Honeywell Normalair-Garrett (Holdings) Limited A method of balancing the supply of bleed air from a plurality of gas turbine engines
EP1413762A3 (en) * 2002-10-23 2004-12-01 Honeywell Normalair-Garrett (Holdings) Limited A method of balancing the supply of bleed air from a plurality of gas turbine engines
US7036319B2 (en) 2002-10-23 2006-05-02 Honeywell Normalair-Garrett (Holdings) Limited Method of balancing the supply of bleed air from a plurality of engines
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
US8276362B2 (en) 2004-12-01 2012-10-02 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
US7854112B2 (en) 2004-12-01 2010-12-21 United Technologies Corporation Vectoring transition duct for turbine engine
US7882694B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Variable fan inlet guide vane assembly for gas turbine engine
US7921635B2 (en) 2004-12-01 2011-04-12 United Technologies Corporation Peripheral combustor for tip turbine engine
US7934902B2 (en) 2004-12-01 2011-05-03 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
US7937927B2 (en) 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
WO2006059982A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Remote engine fuel control and electronic engine control for turbine engine
US7980054B2 (en) 2004-12-01 2011-07-19 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
US8024931B2 (en) 2004-12-01 2011-09-27 United Technologies Corporation Combustor for turbine engine
US9541092B2 (en) 2004-12-01 2017-01-10 United Technologies Corporation Tip turbine engine with reverse core airflow
US8096753B2 (en) 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US9003768B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
US8950171B2 (en) 2004-12-01 2015-02-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
US8561383B2 (en) 2004-12-01 2013-10-22 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
US8641367B2 (en) 2004-12-01 2014-02-04 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
FR2902408A1 (fr) * 2006-06-19 2007-12-21 Eurocopter France Equilibrage en puissance de deux turbomoteurs d'un aeronef
US9346553B2 (en) 2006-06-19 2016-05-24 Airbus Helicopters Balancing the power of two turboshaft engines of an aircraft
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US8489306B2 (en) 2010-05-10 2013-07-16 Rolls-Royce Deutschland Ltd & Co Kg Engine synchronization method
DE102010020024B4 (de) * 2010-05-10 2016-05-25 Rolls-Royce Deutschland Ltd & Co Kg Triebwerkssynchronisierverfahren
DE102010020024A1 (de) * 2010-05-10 2011-11-10 Rolls-Royce Deutschland Ltd & Co Kg Triebwerkssynchronisierverfahren
GB2524775A (en) * 2014-04-02 2015-10-07 Rolls Royce Plc Aircraft vapour trail control system
US9440746B2 (en) 2014-04-02 2016-09-13 Rolls-Royce Plc Aircraft vapour trail control system
GB2524775B (en) * 2014-04-02 2017-11-15 Rolls Royce Plc Aircraft vapour trail control system
US10801361B2 (en) 2016-09-09 2020-10-13 General Electric Company System and method for HPT disk over speed prevention

Also Published As

Publication number Publication date
DE3201010A1 (de) 1982-10-07
FR2502697A1 (fr) 1982-10-01
CA1161527A (en) 1984-01-31
IT8220466A0 (it) 1982-03-30
BR8201832A (pt) 1983-03-01
SE8107800L (sv) 1982-10-01
IT1151860B (it) 1986-12-24
JPS57165632A (en) 1982-10-12

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)