BE837177A - Dispositif d'allumage pour moteur a turbine a gaz - Google Patents

Dispositif d'allumage pour moteur a turbine a gaz

Info

Publication number
BE837177A
BE837177A BE163193A BE163193A BE837177A BE 837177 A BE837177 A BE 837177A BE 163193 A BE163193 A BE 163193A BE 163193 A BE163193 A BE 163193A BE 837177 A BE837177 A BE 837177A
Authority
BE
Belgium
Prior art keywords
gas turbine
turbine engine
ignition device
ignition
engine
Prior art date
Application number
BE163193A
Other languages
English (en)
French (fr)
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 BE837177A publication Critical patent/BE837177A/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

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)
BE163193A 1974-12-30 1975-12-30 Dispositif d'allumage pour moteur a turbine a gaz BE837177A (fr)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
BE837177A true BE837177A (fr) 1976-04-16

Family

ID=24141922

Family Applications (1)

Application Number Title Priority Date Filing Date
BE163193A BE837177A (fr) 1974-12-30 1975-12-30 Dispositif d'allumage pour moteur a turbine a gaz

Country Status (6)

Country Link
JP (1) JPS5198417A (it)
BE (1) BE837177A (it)
DE (1) DE2558756A1 (it)
FR (1) FR2296765A1 (it)
GB (2) GB1537279A (it)
IT (1) IT1052012B (it)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022152989A1 (fr) * 2021-01-15 2022-07-21 Safran Helicopter Engines Procédé et dispositif d'allumage

Families Citing this family (11)

* 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
RU2233989C1 (ru) * 2003-05-30 2004-08-10 Государственное унитарное предприятие Тушинское машиностроительное конструкторское бюро "Союз" - дочернее предприятие Федерального государственного унитарного предприятия "Российская самолетостроительная корпорация "МиГ" Способ и система для запуска газотурбинного двигателя
US7355300B2 (en) 2004-06-15 2008-04-08 Woodward Governor Company Solid state turbine engine ignition exciter having elevated temperature operational capability
RU2362031C2 (ru) * 2007-09-26 2009-07-20 Открытое акционерное общество "Электропривод" Электростартер для запуска газотурбинных установок
FR2988435B1 (fr) * 2012-03-23 2016-03-18 Snecma Boitier d'allumage pour turboreacteur a segregation 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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022152989A1 (fr) * 2021-01-15 2022-07-21 Safran Helicopter Engines Procédé et dispositif d'allumage
FR3118994A1 (fr) * 2021-01-15 2022-07-22 Safran Helicopter Engines Procede et dispositif d’allumage
US12055101B2 (en) 2021-01-15 2024-08-06 Safran Helicopter Engines Ignition method and device

Also Published As

Publication number Publication date
GB1537278A (en) 1978-12-29
JPS5198417A (it) 1976-08-30
GB1537279A (en) 1978-12-29
DE2558756A1 (de) 1976-07-08
FR2296765A1 (fr) 1976-07-30
IT1052012B (it) 1981-06-20

Similar Documents

Publication Publication Date Title
FR2290350A1 (fr) Nacelle pour moteur a turbine a gaz
BE861363A (fr) Diffuseur perfectionne pour moteur a turbine a gaz
FR2333953A1 (fr) Dispositif de reglage de jeu pour un moteur a turbine a gaz
FR2406726B1 (fr) Appareillage de combustion perfectionne pour moteur a turbine a gaz
BE818213A (fr) Dispositif d'alimentation en carburant pour moteur a turbine a gaz
BE810491A (fr) Moteur a turbine a gaz a dispositif de post-combustion
CA1013153A (en) Combustion apparatus for a gas turbine engine
BE825926A (fr) Procede d'equilibrage d'un moteur a turbine a gaz
FR2333957A1 (fr) Dispositif d'allumage par etincelles, notamment pour moteur a turbine a gaz
BE810794A (fr) Moteur a turbine a gaz a dispositif de post-combustion
FR2333126A1 (fr) Dispositif de refrigeration pour chambre de combustion de moteur a turbine a gaz
FR2315612A1 (fr) Moteur a turbine a gaz
FR2309727A1 (fr) Dispositif d'ejection manoeuvrable en vol pour moteur a turbine a gaz
FR2460390B1 (fr) Diffuseur pour moteur a turbine a gaz
FR2293593A1 (fr) Dispositif d'etancheite pour recuperateur de turbines a gaz
FR2317501A1 (fr) Dispositif d'accouplement pour moteur a turbine a gaz
BE856540A (fr) Regulateur de poussee pour un moteur a turbine a gaz
FR2335701A1 (fr) Rotor en ceramique pour moteur a turbine a gaz
FR2316447A1 (fr) Dispositif d'ejection pour un moteur a turbine a gaz
FR2296765A1 (fr) Dispositif d'allumage pour moteur a turbine a gaz
FR2287585A1 (fr) Injecteur de carburant pour moteur a turbine a gaz
BE805378A (fr) Dispositif d'allumage pour moteur a turbine a gaz
FR2314361A1 (fr) Moteur a turbine a gaz
FR2299508A1 (fr) Dispositif de regulation de composition des gaz pour moteur a combustion interne
FR2318323A1 (fr) Dispositif d'allumage pour moteurs a combustion interne