BE686591A - - Google Patents

Info

Publication number
BE686591A
BE686591A BE686591A BE686591A BE686591A BE 686591 A BE686591 A BE 686591A BE 686591 A BE686591 A BE 686591A BE 686591 A BE686591 A BE 686591A BE 686591 A BE686591 A BE 686591A
Authority
BE
Belgium
Application number
BE686591A
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 filed Critical
Publication of BE686591A publication Critical patent/BE686591A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • F02C7/262Restarting after flame-out
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • F02C7/264Ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/30Control parameters, e.g. input parameters
    • F05D2270/303Temperature

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Eletrric Generators (AREA)
BE686591A 1965-09-08 1966-09-08 BE686591A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US485678A US3365881A (en) 1965-09-08 1965-09-08 Gas turbine ignition detector

Publications (1)

Publication Number Publication Date
BE686591A true BE686591A (de) 1967-02-15

Family

ID=23929043

Family Applications (1)

Application Number Title Priority Date Filing Date
BE686591A BE686591A (de) 1965-09-08 1966-09-08

Country Status (8)

Country Link
US (1) US3365881A (de)
BE (1) BE686591A (de)
CH (1) CH462545A (de)
DE (1) DE1476925B2 (de)
FR (1) FR1491893A (de)
GB (1) GB1154641A (de)
NL (1) NL6612581A (de)
SE (1) SE338210B (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3470691A (en) * 1968-06-17 1969-10-07 Avco Corp Automatic starting and protection system for a gas turbine
GB1340879A (en) * 1970-08-11 1973-12-19 Secr Defence Control system for gas turbine engine
US3815561A (en) * 1972-09-14 1974-06-11 Bendix Corp Closed loop engine control system
US3922849A (en) * 1973-10-09 1975-12-02 Aerojet General Co Injector for gas turbine combustor
US4070144A (en) * 1976-01-30 1978-01-24 General Electric Company Control system
DE3408397A1 (de) * 1984-03-08 1985-09-19 Ruhrgas Ag, 4300 Essen Verfahren und anordnung zur bestimmung des mischungsverhaeltnisses eines ein sauerstofftraegergas und einen brennstoff enthaltenden gemisches
JP2006083730A (ja) * 2004-09-15 2006-03-30 Hitachi Ltd ガスタービンの着火検出方法
FR3002284B1 (fr) * 2013-02-18 2015-02-13 Turbomeca Procede de surveillance d'un degre de colmatage d'injecteurs de demarrage d'une turbomachine
FR3118994B1 (fr) * 2021-01-15 2022-12-23 Safran Helicopter Engines Procede et dispositif d’allumage
CN114718736B (zh) * 2022-05-13 2024-05-17 哈尔滨工程大学 一种适用于不同环境下的燃气轮机最佳点火位置调控方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2694899A (en) * 1950-06-09 1954-11-23 Westinghouse Electric Corp Liquid fuel vaporizing apparatus
US2888801A (en) * 1951-03-13 1959-06-02 Garrett Corp Power plant starting system
US2866385A (en) * 1956-01-10 1958-12-30 Northrop Aircraft Inc Automatic jet engine starting device
US2928002A (en) * 1956-03-06 1960-03-08 Itt Amplitude sensitive circuit

Also Published As

Publication number Publication date
DE1476925A1 (de) 1970-04-02
NL6612581A (de) 1967-03-09
GB1154641A (en) 1969-06-11
FR1491893A (fr) 1967-08-11
US3365881A (en) 1968-01-30
CH462545A (de) 1968-09-15
SE338210B (de) 1971-08-30
DE1476925B2 (de) 1972-02-10

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Legal Events

Date Code Title Description
RE20 Patent expired

Owner name: UNITED AIRCRAFT CORP.

Effective date: 19860908