BE698806A - Dispositif indicateur de température pour moteurs à turbine à gaz - Google Patents

Dispositif indicateur de température pour moteurs à turbine à gaz

Info

Publication number
BE698806A
BE698806A BE698806DA BE698806A BE 698806 A BE698806 A BE 698806A BE 698806D A BE698806D A BE 698806DA BE 698806 A BE698806 A BE 698806A
Authority
BE
Belgium
Prior art keywords
gas turbine
indicating device
turbine engines
temperature indicating
temperature
Prior art date
Application number
Other languages
English (en)
Inventor
Ira E Marvin
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 BE698806A publication Critical patent/BE698806A/fr

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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/02—Arrangement of sensing elements
    • F01D17/08—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure
    • F01D17/085—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure to temperature
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K13/00—Thermometers specially adapted for specific purposes
    • G01K13/02—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
    • G01K7/00—Measuring temperature based on the use of electric or magnetic elements directly sensitive to heat ; Power supply therefor, e.g. using thermoelectric elements
    • 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
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Measuring Volume Flow (AREA)
BE698806D 1966-08-22 1967-05-22 Dispositif indicateur de température pour moteurs à turbine à gaz BE698806A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US574140A US3377848A (en) 1966-08-22 1966-08-22 Temperature indicating means for gas turbine engines

Publications (1)

Publication Number Publication Date
BE698806A true BE698806A (fr) 1967-11-03

Family

ID=24294852

Family Applications (1)

Application Number Title Priority Date Filing Date
BE698806D BE698806A (fr) 1966-08-22 1967-05-22 Dispositif indicateur de température pour moteurs à turbine à gaz

Country Status (4)

Country Link
US (1) US3377848A (fr)
BE (1) BE698806A (fr)
DE (1) DE1601556A1 (fr)
GB (1) GB1159837A (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3492814A (en) * 1968-02-13 1970-02-03 United Aircraft Corp Fuel control
US4425614A (en) 1969-12-09 1984-01-10 Adaptronics, Inc. Self-organizing control system
US3808882A (en) * 1971-07-21 1974-05-07 Dresser Ind Engine torque control system
US3789665A (en) * 1972-02-22 1974-02-05 Avco Corp Inferred measurement of the turbine inlet temperature of a gas turbine engine
GB1415681A (en) * 1972-06-24 1975-11-26 Rolls Royce Flame-out control in gas turbine engine
US4115998A (en) * 1975-12-08 1978-09-26 General Electric Company Combustion monitor
US4058975A (en) * 1975-12-08 1977-11-22 General Electric Company Gas turbine temperature sensor validation apparatus and method
US4055997A (en) * 1976-09-15 1977-11-01 United Technologies Corporation Means for calculating turbine inlet temperature of a gas turbine engine
GB2011091B (en) * 1977-12-22 1982-04-28 Gen Electric Method and apparatus for calculating turbine inlet temperature
US4336713A (en) * 1980-08-06 1982-06-29 The United States Of America As Represented By The Secretary Of The Air Force Compensated temperature sensing device
US4744670A (en) * 1986-05-05 1988-05-17 Honeywell, Inc. Method and apparatus for monitoring the temperature of the propulsion gas at the inlet to a high-performance turbine wheel
US4748804A (en) * 1986-12-08 1988-06-07 United Technologies Corporation Inlet total temperature synthesis for gas turbine engines
US5080496A (en) * 1990-06-25 1992-01-14 General Electric Company Method and apparatus for compensated temperature prediction
JPH07189741A (ja) * 1993-12-10 1995-07-28 Solar Turbines Inc 燃焼室１次ゾーン温度決定制御装置及び方法
GB9410760D0 (en) * 1994-05-27 1994-07-27 Rolls Royce Plc Gas turbine engine fuel control system
US5622042A (en) * 1995-02-27 1997-04-22 Compressor Controls Corporation Method for predicting and using the exhaust gas temperatures for control of two and three shaft gas turbines
GB0221866D0 (en) * 2002-09-20 2002-10-30 Turbintel Ltd System and method for measuring one or more properties of a gas
US6952639B2 (en) * 2002-11-12 2005-10-04 General Electric Company Method and system for temperature estimation of gas turbine combustion cans
GB2397395B (en) * 2003-01-16 2006-04-05 Rolls Royce Plc Controlling the fuel supply to a combustor of a gas turbine engine
US6931857B2 (en) 2003-05-30 2005-08-23 United Technologies Corporation Rotor inlet temperature control for turbo machine
EP1655590B1 (fr) * 2004-11-09 2016-02-03 Alstom Technology Ltd Procédé destiné à déterminer la température, calculée sur la masse d'une section d'un flux de gaz dans une turbine à gaz
CA2626035C (fr) 2005-10-18 2014-12-02 Alstom Technology Ltd Methode de protection des parties de gaz chaudes d'une installation a turbine a gaz contre une surchauffe et de detection d'une extinction de flamme dans la chambre de combustion
US20080254302A1 (en) * 2007-04-13 2008-10-16 David Paul Bourcier Multiple layer polymer interlayers having a melt fractured surface
US8321120B2 (en) * 2009-01-16 2012-11-27 Honeywell International Inc. System and method for starting a gas turbine engine with inoperable exhaust gas turbine temperature sensor

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2809492A (en) * 1952-12-23 1957-10-15 Simmonds Aerocessories Inc Apparatus for measuring and/or controlling fuel/air ratio of gas turbines without direct gravimetric fuel metering
US2836976A (en) * 1953-08-13 1958-06-03 Sulzer Ag Determining and controlling the inlet temperature of a gas turbine
US3025670A (en) * 1957-03-07 1962-03-20 Allen S Atkinson Method and apparatus for detecting, measuring and controlling the temperature of gas turbine engines
GB906592A (en) * 1959-01-22 1962-09-26 Power Jets Res & Dev Ltd Control systems for aircraft gas turbine engines

Also Published As

Publication number Publication date
US3377848A (en) 1968-04-16
GB1159837A (en) 1969-07-30
DE1601556A1 (de) 1970-02-26

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