FR1105427A - Ignition device for starting a gas turbine engine - Google Patents

Ignition device for starting a gas turbine engine

Info

Publication number
FR1105427A
FR1105427A FR1105427DA FR1105427A FR 1105427 A FR1105427 A FR 1105427A FR 1105427D A FR1105427D A FR 1105427DA FR 1105427 A FR1105427 A FR 1105427A
Authority
FR
France
Prior art keywords
starting
gas turbine
turbine engine
ignition device
ignition
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
Other languages
French (fr)
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Application granted granted Critical
Publication of FR1105427A publication Critical patent/FR1105427A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • F23R3/343Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Gas Burners (AREA)
FR1105427D 1953-08-01 1954-07-26 Ignition device for starting a gas turbine engine Expired FR1105427A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2140853A GB743809A (en) 1953-08-01 1953-08-01 Ignition means for use in starting gas turbine engines

Publications (1)

Publication Number Publication Date
FR1105427A true FR1105427A (en) 1955-12-02

Family

ID=10162437

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1105427D Expired FR1105427A (en) 1953-08-01 1954-07-26 Ignition device for starting a gas turbine engine

Country Status (4)

Country Link
BE (1) BE530786A (en)
DE (1) DE1003515B (en)
FR (1) FR1105427A (en)
GB (1) GB743809A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4161102A (en) * 1977-10-05 1979-07-17 Teledyne Industries, Inc. Turbine engine starting system
DE10108561A1 (en) * 2001-02-22 2002-09-05 Alstom Switzerland Ltd Thermal turbomachine and method for igniting the thermal turbomachine
CN114151200A (en) * 2021-10-20 2022-03-08 中国航发四川燃气涡轮研究院 Igniter

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB628366A (en) * 1947-09-01 1949-08-26 Donald Louis Mordell Improvements relating to gas turbine engines
GB655121A (en) * 1948-05-19 1951-07-11 Rolls Royce Improvements relating to ignition means for gas-turbine engines
GB686131A (en) * 1950-06-29 1953-01-21 Rolls Royce Improvements in or relating to ignition arrangements for gas-turbine engines

Also Published As

Publication number Publication date
DE1003515B (en) 1957-02-28
GB743809A (en) 1956-01-25
BE530786A (en)

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