CA974629A - Gas turbine starting and operating system - Google Patents

Gas turbine starting and operating system

Info

Publication number
CA974629A
CA974629A CA159,301A CA159301A CA974629A CA 974629 A CA974629 A CA 974629A CA 159301 A CA159301 A CA 159301A CA 974629 A CA974629 A CA 974629A
Authority
CA
Canada
Prior art keywords
operating system
gas turbine
turbine starting
starting
gas
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.)
Expired
Application number
CA159,301A
Other versions
CA159301S (en
Inventor
James E. Fenton
Irwin C. Dickhart
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.)
Ford Motor Company of Canada Ltd
Original Assignee
Ford Motor Company of Canada Ltd
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 Ford Motor Company of Canada Ltd filed Critical Ford Motor Company of Canada Ltd
Application granted granted Critical
Publication of CA974629A publication Critical patent/CA974629A/en
Expired legal-status Critical Current

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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/262—Restarting after flame-out
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
CA159,301A 1972-01-27 1972-12-18 Gas turbine starting and operating system Expired CA974629A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US22132572A 1972-01-27 1972-01-27

Publications (1)

Publication Number Publication Date
CA974629A true CA974629A (en) 1975-09-16

Family

ID=22827342

Family Applications (1)

Application Number Title Priority Date Filing Date
CA159,301A Expired CA974629A (en) 1972-01-27 1972-12-18 Gas turbine starting and operating system

Country Status (2)

Country Link
US (1) US3793825A (en)
CA (1) CA974629A (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4019315A (en) * 1973-06-20 1977-04-26 Westinghouse Electric Corporation Gas turbine power plant control apparatus including a temperature reset starting control system and an ignition pressure control system
US4350008A (en) * 1979-12-26 1982-09-21 United Technologies Corporation Method of starting turbine engines
DE4221805A1 (en) * 1992-07-03 1994-01-05 Mak System Gmbh Starting control for gas turbine engine - has electronic control for progressive start=up with intermediate speed and final operating speed
US5917416A (en) * 1997-03-11 1999-06-29 Read; Robert Michael Easy to install temperature alarm system
US6018941A (en) 1997-09-19 2000-02-01 Lamar Technologies Corporation Electric starter system for turbine aircraft engines
US20140165586A1 (en) * 2012-12-17 2014-06-19 United Technologies Corporation Turbine start method
US9157372B2 (en) 2013-03-11 2015-10-13 Bell Helicopter Textron Inc. Series battery start controller
US9611752B2 (en) 2013-03-15 2017-04-04 General Electric Company Compressor start bleed system for a turbine system and method of controlling a compressor start bleed system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3097485A (en) * 1963-07-16 bidwell
US2880790A (en) * 1951-08-10 1959-04-07 Bendix Aviat Corp Starting fuel control for gas turbine engines
US2730862A (en) * 1951-10-03 1956-01-17 Zenith Carburateur Soc Du Electric ignition control in starting devices for turbo-engines
NL251582A (en) * 1959-05-15
US3197958A (en) * 1961-10-11 1965-08-03 Parker Hannifin Corp Fuel selector and flow divider valve and control means for jet engines
FR1388004A (en) * 1963-11-27 1965-02-05 Device for starting and controlling the operation of a gas turbine power generator
US3282323A (en) * 1965-04-14 1966-11-01 Gen Electric Viscosity responsive devices

Also Published As

Publication number Publication date
US3793825A (en) 1974-02-26

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