IT1100560B - Metodo ed apparato per calcolare la temperatura di ingresso di una turbina - Google Patents

Metodo ed apparato per calcolare la temperatura di ingresso di una turbina

Info

Publication number
IT1100560B
IT1100560B IT29989/78A IT2998978A IT1100560B IT 1100560 B IT1100560 B IT 1100560B IT 29989/78 A IT29989/78 A IT 29989/78A IT 2998978 A IT2998978 A IT 2998978A IT 1100560 B IT1100560 B IT 1100560B
Authority
IT
Italy
Prior art keywords
turbine
calculate
inlet temperature
inlet
temperature
Prior art date
Application number
IT29989/78A
Other languages
English (en)
Other versions
IT7829989A0 (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 IT7829989A0 publication Critical patent/IT7829989A0/it
Application granted granted Critical
Publication of IT1100560B publication Critical patent/IT1100560B/it

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

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)
  • Investigating Or Analyzing Materials Using Thermal Means (AREA)
IT29989/78A 1977-12-22 1978-11-21 Metodo ed apparato per calcolare la temperatura di ingresso di una turbina IT1100560B (it)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
IT7829989A0 IT7829989A0 (it) 1978-11-21
IT1100560B true IT1100560B (it) 1985-09-28

Family

ID=25341170

Family Applications (1)

Application Number Title Priority Date Filing Date
IT29989/78A IT1100560B (it) 1977-12-22 1978-11-21 Metodo ed apparato per calcolare la temperatura di ingresso di una turbina

Country Status (5)

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

Families Citing this family (11)

* 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
JP2004132255A (ja) 2002-10-10 2004-04-30 Mitsubishi Heavy Ind Ltd 燃焼器制御装置
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
CA2626035C (en) 2005-10-18 2014-12-02 Alstom Technology Ltd Method for protecting the hot gas parts of a gas turbine installation from overheating and for detecting flame extinction in the combustion chamber
CN100365256C (zh) * 2005-12-26 2008-01-30 王菲 脉动式燃气轮机
DE102006037560B4 (de) * 2006-02-06 2008-06-19 Siemens Ag Verfahren und Vorrichtung zum vorausschauenden Bestimmen einer Temperaturverteilung in einer Wand einer Turbinenanlage
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 (zh) * 2021-07-05 2022-04-22 中国航发湖南动力机械研究所 一种用于控制系统的燃气涡轮前温度计算方法

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

Also Published As

Publication number Publication date
FR2412891B1 (it) 1984-06-22
DE2850625A1 (de) 1979-06-28
JPS5490409A (en) 1979-07-18
GB2011091B (en) 1982-04-28
IT7829989A0 (it) 1978-11-21
FR2412891A1 (fr) 1979-07-20
GB2011091A (en) 1979-07-04

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