JPS5490409A - Temperature indicating apparatus and method - Google Patents

Temperature indicating apparatus and method

Info

Publication number
JPS5490409A
JPS5490409A JP14348478A JP14348478A JPS5490409A JP S5490409 A JPS5490409 A JP S5490409A JP 14348478 A JP14348478 A JP 14348478A JP 14348478 A JP14348478 A JP 14348478A JP S5490409 A JPS5490409 A JP S5490409A
Authority
JP
Japan
Prior art keywords
temperature indicating
indicating apparatus
temperature
indicating
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.)
Pending
Application number
JP14348478A
Other languages
Japanese (ja)
Inventor
Edowaado Maabin Aira
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
Publication of JPS5490409A publication Critical patent/JPS5490409A/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • G01K13/028—Thermometers specially adapted for specific purposes for measuring temperature of moving fluids or granular materials capable of flow for use in total air temperature [TAT] probes
    • 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
    • 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
    • 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
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
JP14348478A 1977-12-22 1978-11-22 Temperature indicating apparatus and method Pending JPS5490409A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US86348377A 1977-12-22 1977-12-22

Publications (1)

Publication Number Publication Date
JPS5490409A true JPS5490409A (en) 1979-07-18

Family

ID=25341170

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14348478A Pending JPS5490409A (en) 1977-12-22 1978-11-22 Temperature indicating apparatus and method

Country Status (5)

Country Link
JP (1) JPS5490409A (en)
DE (1) DE2850625A1 (en)
FR (1) FR2412891A1 (en)
GB (1) GB2011091B (en)
IT (1) IT1100560B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7191588B2 (en) 2002-10-10 2007-03-20 Mitsubishi Heavy Industries, Ltd Combustor controller

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4748804A (en) * 1986-12-08 1988-06-07 United Technologies Corporation Inlet total temperature synthesis for gas turbine engines
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
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
JP4990902B2 (en) 2005-10-18 2012-08-01 アルストム テクノロジー リミテッド Method for protecting a gas turbine device from overheating of the part guiding the hot gas and detecting the disappearance of the flame in the combustion chamber
CN100365256C (en) * 2005-12-26 2008-01-30 王菲 Pulsating flow gas turbine
DE102006037560B4 (en) * 2006-02-06 2008-06-19 Siemens Ag Method and device for predictive determination of a temperature distribution in a wall of a turbine plant
EP2357339A1 (en) 2010-02-12 2011-08-17 Siemens Aktiengesellschaft Method of determining a combustor exit temperature and method of controlling a gas turbine
CN113378328B (en) * 2021-07-05 2022-04-22 中国航发湖南动力机械研究所 Gas turbine front temperature calculation method for control system

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
US3377848A (en) * 1966-08-22 1968-04-16 Gen Electric Temperature indicating means for gas turbine engines
US3789665A (en) * 1972-02-22 1974-02-05 Avco Corp Inferred measurement of the turbine inlet temperature of a gas turbine engine
US4055997A (en) * 1976-09-15 1977-11-01 United Technologies Corporation Means for calculating turbine inlet temperature of a gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7191588B2 (en) 2002-10-10 2007-03-20 Mitsubishi Heavy Industries, Ltd Combustor controller

Also Published As

Publication number Publication date
GB2011091B (en) 1982-04-28
FR2412891B1 (en) 1984-06-22
IT7829989A0 (en) 1978-11-21
FR2412891A1 (en) 1979-07-20
IT1100560B (en) 1985-09-28
DE2850625A1 (en) 1979-06-28
GB2011091A (en) 1979-07-04

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