IT1052012B - Sistema di accensione per turbomotore a gas - Google Patents

Sistema di accensione per turbomotore a gas

Info

Publication number
IT1052012B
IT1052012B IT3083275A IT3083275A IT1052012B IT 1052012 B IT1052012 B IT 1052012B IT 3083275 A IT3083275 A IT 3083275A IT 3083275 A IT3083275 A IT 3083275A IT 1052012 B IT1052012 B IT 1052012B
Authority
IT
Italy
Prior art keywords
ignition system
turbo engine
gas turbo
engine
gas
Prior art date
Application number
IT3083275A
Other languages
English (en)
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
Application granted granted Critical
Publication of IT1052012B publication Critical patent/IT1052012B/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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
IT3083275A 1974-12-30 1975-12-30 Sistema di accensione per turbomotore a gas IT1052012B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US53726474A 1974-12-30 1974-12-30

Publications (1)

Publication Number Publication Date
IT1052012B true IT1052012B (it) 1981-06-20

Family

ID=24141922

Family Applications (1)

Application Number Title Priority Date Filing Date
IT3083275A IT1052012B (it) 1974-12-30 1975-12-30 Sistema di accensione per turbomotore a gas

Country Status (6)

Country Link
JP (1) JPS5198417A (it)
BE (1) BE837177A (it)
DE (1) DE2558756A1 (it)
FR (1) FR2296765A1 (it)
GB (2) GB1537278A (it)
IT (1) IT1052012B (it)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2722449C2 (de) * 1977-05-18 1982-08-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Zündeinrichtung einer Brennkammer für Gasturbinentriebwerke, insbesondere für Gasturbinenstrahltriebwerke von Flugzeugen
FR2496762B1 (fr) * 1980-12-24 1985-06-28 Psa Grpt Int Eco Rech Develop Dispositif d'allumage et de reallumage pour turbine a gaz
US5245252A (en) 1988-11-15 1993-09-14 Frus John R Apparatus and method for providing ignition to a turbine engine
US5523691A (en) * 1990-07-26 1996-06-04 Unison Industries Limited Partnership Diagnostic device for gas turbine ignition system
US5155437A (en) * 1990-07-26 1992-10-13 Unison Industries Limited Partnership Diagnostic device for gas turbine ignition system
US5754011A (en) 1995-07-14 1998-05-19 Unison Industries Limited Partnership Method and apparatus for controllably generating sparks in an ignition system or the like
US6670777B1 (en) 2002-06-28 2003-12-30 Woodward Governor Company Ignition system and method
FR2988435B1 (fr) * 2012-03-23 2016-03-18 Snecma Boitier d'allumage pour turboreacteur a segregation d'allumage
FR3118994B1 (fr) * 2021-01-15 2022-12-23 Safran Helicopter Engines Procede et dispositif d’allumage

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB701659A (en) * 1950-10-11 1953-12-30 Carburation Pour L Automobile Improvements in or relating to electric ignition starting devices for gas turbine engines
US2881587A (en) * 1955-08-23 1959-04-14 Bendix Aviat Corp Electrical apparatus having means to control the supply of energy from a coil to a plurality of circuits
US2938147A (en) * 1959-02-17 1960-05-24 John J Rose Continuous ignition system for a turbojet engine
FR1319068A (fr) * 1961-04-07 1963-02-22 Rolls Royce Chambre de combustion d'un turbo-moteur à gaz
US3041833A (en) * 1961-07-06 1962-07-03 Paul J Vore Turbo jet and turbo prop engine relite device
GB1340879A (en) * 1970-08-11 1973-12-19 Secr Defence Control system for gas turbine engine
US3765176A (en) * 1972-02-22 1973-10-16 Gen Motors Corp Automatic relight
GB1415681A (en) * 1972-06-24 1975-11-26 Rolls Royce Flame-out control in gas turbine engine
US3793826A (en) * 1972-12-08 1974-02-26 Gen Motors Corp Electronic start control circuit for gas turbine engine

Also Published As

Publication number Publication date
GB1537279A (en) 1978-12-29
FR2296765A1 (fr) 1976-07-30
BE837177A (fr) 1976-04-16
JPS5198417A (it) 1976-08-30
GB1537278A (en) 1978-12-29
DE2558756A1 (de) 1976-07-08

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