IT8024211A0 - Sistema di controllo privo di regolatore per il combustibile di turbine a gas. - Google Patents

Sistema di controllo privo di regolatore per il combustibile di turbine a gas.

Info

Publication number
IT8024211A0
IT8024211A0 IT8024211A IT2421180A IT8024211A0 IT 8024211 A0 IT8024211 A0 IT 8024211A0 IT 8024211 A IT8024211 A IT 8024211A IT 2421180 A IT2421180 A IT 2421180A IT 8024211 A0 IT8024211 A0 IT 8024211A0
Authority
IT
Italy
Prior art keywords
regulator
control system
gas turbine
free control
turbine fuel
Prior art date
Application number
IT8024211A
Other languages
English (en)
Other versions
IT1132431B (it
Inventor
Charles F Stearns
David L Chapski
Kenneth F Vosseller
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of IT8024211A0 publication Critical patent/IT8024211A0/it
Application granted granted Critical
Publication of IT1132431B publication Critical patent/IT1132431B/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
IT24211/80A 1979-08-23 1980-08-19 Sistema di controllo privo di regolatore per il combustibile di turbine a gas IT1132431B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/069,141 US4326376A (en) 1979-08-23 1979-08-23 Governorless gas turbine fuel control

Publications (2)

Publication Number Publication Date
IT8024211A0 true IT8024211A0 (it) 1980-08-19
IT1132431B IT1132431B (it) 1986-07-02

Family

ID=22087009

Family Applications (1)

Application Number Title Priority Date Filing Date
IT24211/80A IT1132431B (it) 1979-08-23 1980-08-19 Sistema di controllo privo di regolatore per il combustibile di turbine a gas

Country Status (9)

Country Link
US (1) US4326376A (it)
JP (1) JPS56167821A (it)
CA (1) CA1143036A (it)
DE (1) DE3030466A1 (it)
FR (1) FR2463855B1 (it)
GB (1) GB2057577B (it)
IL (1) IL60795A (it)
IT (1) IT1132431B (it)
SE (1) SE445660B (it)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4422287A (en) * 1980-09-29 1983-12-27 United Technologies Corporation Fuel control for gas turbine engines
US4411133A (en) * 1980-09-29 1983-10-25 United Technologies Corporation Fuel circuits for fuel controls
GB9122965D0 (en) * 1991-10-29 1991-12-18 Rolls Royce Plc Turbine engine control system
FR2685384A1 (fr) * 1991-12-18 1993-06-25 Snecma Systeme d'alimentation en carburant des injecteurs d'une turbomachine.
GB0408886D0 (en) * 2004-04-22 2004-05-26 Rolls Royce Plc Fuel metering unit
CH698104B1 (de) * 2004-11-03 2009-05-29 Alstom Technology Ltd Brennstoffdrosselventil zum Betreiben einer Brenneranordnung einer Gasturbine sowie Brenneranordnung mit Brennstoffdrosselventil.
US7818970B2 (en) 2005-09-12 2010-10-26 Rolls-Royce Power Engineering Plc Controlling a gas turbine engine with a transient load
US9115648B2 (en) * 2009-04-10 2015-08-25 General Electric Company Corrected megawatt backup curve methodology
US8381530B2 (en) * 2009-04-28 2013-02-26 General Electric Company System and method for controlling combustion dynamics
US10801361B2 (en) 2016-09-09 2020-10-13 General Electric Company System and method for HPT disk over speed prevention
US11280683B2 (en) 2017-05-31 2022-03-22 Pratt & Whitney Canada Corp. Method and system for detecting high turbine temperature operations
US10233768B1 (en) * 2018-03-22 2019-03-19 Florida Turbine Technologies, Inc. Apparatus and process for optimizing turbine engine performance via load control through a power control module

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE568106A (it) *
US2950597A (en) * 1956-12-05 1960-08-30 Bendix Corp Apparatus for minimum fuel flow scheduling during decheleration of an engine
FR1472828A (fr) * 1966-03-30 1967-03-10 United Aircraft Corp Perfectionnements aux régulateurs de débit de carburant hydrauliques
US3611719A (en) * 1968-07-12 1971-10-12 United Aircraft Corp Fuel control
US3713290A (en) * 1971-05-28 1973-01-30 Nasa Gas turbine engine fuel control
US4078378A (en) * 1976-11-08 1978-03-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Automotive gas turbine fuel control
DE2751743C2 (de) * 1977-11-19 1985-04-18 Pierburg Luftfahrtgeräte Union GmbH, 4040 Neuss Verfahren und Regeleinrichtung zum Zumessen strömender Medien

Also Published As

Publication number Publication date
IL60795A (en) 1982-12-31
IT1132431B (it) 1986-07-02
IL60795A0 (en) 1980-10-26
JPS56167821A (en) 1981-12-23
DE3030466A1 (de) 1981-03-26
JPS648174B2 (it) 1989-02-13
FR2463855A1 (fr) 1981-02-27
SE8005901L (sv) 1981-02-24
DE3030466C2 (it) 1992-05-07
FR2463855B1 (fr) 1986-06-20
SE445660B (sv) 1986-07-07
GB2057577B (en) 1983-02-02
US4326376A (en) 1982-04-27
GB2057577A (en) 1981-04-01
CA1143036A (en) 1983-03-15

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