IT1110712B - Metodo e apparato per controllare la spinta in un turbomotore a gas - Google Patents

Metodo e apparato per controllare la spinta in un turbomotore a gas

Info

Publication number
IT1110712B
IT1110712B IT19518/79A IT1951879A IT1110712B IT 1110712 B IT1110712 B IT 1110712B IT 19518/79 A IT19518/79 A IT 19518/79A IT 1951879 A IT1951879 A IT 1951879A IT 1110712 B IT1110712 B IT 1110712B
Authority
IT
Italy
Prior art keywords
thrust
control
turbo engine
gas turbo
engine
Prior art date
Application number
IT19518/79A
Other languages
English (en)
Other versions
IT7919518A0 (it
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT7919518A0 publication Critical patent/IT7919518A0/it
Application granted granted Critical
Publication of IT1110712B publication Critical patent/IT1110712B/it

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
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/051—Thrust
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
IT19518/79A 1978-01-25 1979-01-23 Metodo e apparato per controllare la spinta in un turbomotore a gas IT1110712B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/872,125 US4275557A (en) 1978-01-25 1978-01-25 Method and apparatus for controlling thrust in a gas turbine engine

Publications (2)

Publication Number Publication Date
IT7919518A0 IT7919518A0 (it) 1979-01-23
IT1110712B true IT1110712B (it) 1986-01-06

Family

ID=25358895

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19518/79A IT1110712B (it) 1978-01-25 1979-01-23 Metodo e apparato per controllare la spinta in un turbomotore a gas

Country Status (6)

Country Link
US (1) US4275557A (it)
JP (1) JPS54112409A (it)
DE (1) DE2902697A1 (it)
FR (1) FR2415724B1 (it)
GB (1) GB2013372B (it)
IT (1) IT1110712B (it)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11236635B2 (en) * 2018-11-02 2022-02-01 Rolls-Royce Plc Gas turbine engine power setting

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57501096A (it) * 1980-06-23 1982-06-24
US4414807A (en) * 1980-12-08 1983-11-15 United Technologies Corporation Method and apparatus for controlling a gas turbine engine
US4928484A (en) * 1988-12-20 1990-05-29 Allied-Signal Inc. Nonlinear multivariable control system
US5163282A (en) * 1991-07-19 1992-11-17 Shell Oil Company Turbine process
US5315819A (en) * 1991-09-17 1994-05-31 Allied-Signal Inc. Power management system for turbine engines
GB2262623B (en) * 1991-12-17 1995-04-26 Rolls Royce Plc Aircraft engine management system
US5447023A (en) * 1992-06-30 1995-09-05 United Technologies Corporation Synthesized fuel flow rate and metering valve position
US6217288B1 (en) * 1998-01-20 2001-04-17 Compressor Controls Corporation Method and apparatus for limiting a critical variable of a group of compressors or an individual compressor
US6171055B1 (en) * 1998-04-03 2001-01-09 Aurora Flight Sciences Corporation Single lever power controller for manned and unmanned aircraft
US9506405B2 (en) 1998-04-03 2016-11-29 Rockwell Collins Control Technologies, Inc. Apparatus and method for controlling power generation system
US7011498B2 (en) * 1998-04-03 2006-03-14 Athena Technologies, Inc. Optimization method for power generation systems
US6487490B1 (en) * 1999-05-26 2002-11-26 General Electric Company Speed modification system for gas turbine engine to allow trimming of excess
US6459963B1 (en) * 2000-07-31 2002-10-01 General Electric Company Methods and apparatus for trimming engine control systems
US7010904B2 (en) * 2003-12-05 2006-03-14 United Technologies Corporation Method for control scheduling to achieve linear thrust response
US20050193739A1 (en) * 2004-03-02 2005-09-08 General Electric Company Model-based control systems and methods for gas turbine engines
US20060129301A1 (en) * 2004-12-14 2006-06-15 General Electric Company Method and apparatus for assessing gas turbine acceleration capability
EP1837506B1 (en) * 2006-03-24 2013-08-28 Rolls-Royce plc Method for monitoring thrust in gas turbine engines
US20070260424A1 (en) * 2006-05-05 2007-11-08 Harold Brown Methods and apparatus for estimating engine thrust
US7861578B2 (en) * 2008-07-29 2011-01-04 General Electric Company Methods and systems for estimating operating parameters of an engine
US9239012B2 (en) 2011-06-08 2016-01-19 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US9631558B2 (en) 2012-01-03 2017-04-25 United Technologies Corporation Geared architecture for high speed and small volume fan drive turbine
US9410608B2 (en) 2011-06-08 2016-08-09 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US8490404B1 (en) * 2012-02-28 2013-07-23 General Electric Company Sensor-based performance-seeking gas turbine engine control
US10125693B2 (en) 2012-04-02 2018-11-13 United Technologies Corporation Geared turbofan engine with power density range
EP2904251B1 (en) 2012-10-01 2019-06-26 United Technologies Corporation Method of defining gas turbine engine control ratings
FR3024755B1 (fr) * 2014-08-08 2019-06-21 Safran Aircraft Engines Hybridation des compresseurs d'un turboreacteur
US10961920B2 (en) 2018-10-02 2021-03-30 8 Rivers Capital, Llc Control systems and methods suitable for use with power production systems and methods
US11686258B2 (en) 2014-11-12 2023-06-27 8 Rivers Capital, Llc Control systems and methods suitable for use with power production systems and methods
US10190440B2 (en) * 2015-06-10 2019-01-29 Rolls-Royce North American Technologies, Inc. Emergency shut-down detection system for a gas turbine
US9828106B2 (en) * 2015-06-18 2017-11-28 Honeywell International Inc. Aircraft gas turbine propulsion engine control without aircraft total air temperature sensors
CN109072783B (zh) * 2016-02-26 2021-08-03 八河流资产有限责任公司 用于控制发电设备的系统和方法
US10473038B2 (en) 2016-10-26 2019-11-12 Pratt & Whitney Canada Corp. Power plant thrust management system for turboprop engines
US11300069B2 (en) * 2018-11-28 2022-04-12 Honeywell International Inc. Self-generating engine-specific health monitoring model from generic model base
US11549433B2 (en) 2019-10-22 2023-01-10 8 Rivers Capital, Llc Control schemes for thermal management of power production systems and methods
US11952944B1 (en) 2023-02-10 2024-04-09 General Electric Company Jet engine thermal transport bus pumps

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3307353A (en) * 1964-01-15 1967-03-07 United Aircraft Corp Fuel control
US3314233A (en) * 1964-01-15 1967-04-18 United Aircraft Corp Fuel control
US3295315A (en) * 1964-05-22 1967-01-03 United Aircraft Corp Fuel control
US3316713A (en) * 1965-12-27 1967-05-02 United Aircraft Corp Closed-loop fuel control for gas turbine engines
JPS4936452B1 (it) * 1970-09-14 1974-10-01
US3764814A (en) * 1972-03-27 1973-10-09 United Aircraft Corp Control for auxiliary power unit
US3832846A (en) * 1972-04-27 1974-09-03 Woodward Governor Co Speed governor with fuel rate control
GB1470757A (en) * 1973-04-27 1977-04-21 Lucas Industries Ltd Fuel control systems for gas turbine engines
US3797233A (en) * 1973-06-28 1974-03-19 United Aircraft Corp Integrated control for a turbopropulsion system
US3854287A (en) * 1973-12-26 1974-12-17 United Aircraft Corp Self-trimming control for turbofan engines
US3936226A (en) * 1974-06-07 1976-02-03 United Technologies Corporation Control system for variable pitch fan propulsor with reverse pitch
US3902315A (en) * 1974-06-12 1975-09-02 United Aircraft Corp Starting fuel control system for gas turbine engines
US4060980A (en) * 1975-11-19 1977-12-06 United Technologies Corporation Stall detector for a gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11236635B2 (en) * 2018-11-02 2022-02-01 Rolls-Royce Plc Gas turbine engine power setting

Also Published As

Publication number Publication date
GB2013372A (en) 1979-08-08
DE2902697A1 (de) 1979-07-26
JPS6132484B2 (it) 1986-07-28
IT7919518A0 (it) 1979-01-23
JPS54112409A (en) 1979-09-03
FR2415724B1 (fr) 1986-03-14
GB2013372B (en) 1982-06-03
US4275557A (en) 1981-06-30
FR2415724A1 (fr) 1979-08-24

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