GB714596A - Improvements relating to ignition means for combustion chambers, particularly for use in gas turbine plant - Google Patents

Improvements relating to ignition means for combustion chambers, particularly for use in gas turbine plant

Info

Publication number
GB714596A
GB714596A GB2155151A GB2155151A GB714596A GB 714596 A GB714596 A GB 714596A GB 2155151 A GB2155151 A GB 2155151A GB 2155151 A GB2155151 A GB 2155151A GB 714596 A GB714596 A GB 714596A
Authority
GB
United Kingdom
Prior art keywords
igniter
gas turbine
spray nozzle
combustion chambers
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
GB2155151A
Inventor
James Hodge
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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
Priority to BE513952D priority Critical patent/BE513952A/xx
Application filed by Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB2155151A priority patent/GB714596A/en
Priority to FR1068816D priority patent/FR1068816A/en
Priority to CH308091D priority patent/CH308091A/en
Publication of GB714596A publication Critical patent/GB714596A/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
    • F02C7/264—Ignition

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

714,596. Igniting burners. POWER JETS (RESEARCH AND DEVELOPMENT), Ltd. Aug. 29, 1952 [Sept. 13, 1951], No. 21551/51. Classes 75 (1) and 75 (3) For igniting fuel injected through a spray nozzle 3 into a flame tube 2 within a combustion chamber 1 of a gas turbine engine, a gas igniter torch 4 is inserted through apertures in the members 1, 2 normally closed by spring urged flaps 12, 14 which are pushed open by the end of the igniter 4. The latter is supplied from a container 6 of compressed gas through a flexible pipe 5 and is provided with a stop 10 which may be adjustable and which limits the insertion into the chamber 1. A flame guard 9 prevents extinction of the igniter during insertion and may be retractable to facilitate ignition of the main fuel. If instead of the spray nozzle 3 a vaporizer tube combustion system is employed, the igniter serves also to preheat the vaporizer tubes.
GB2155151A 1951-09-13 1951-09-13 Improvements relating to ignition means for combustion chambers, particularly for use in gas turbine plant Expired GB714596A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BE513952D BE513952A (en) 1951-09-13
GB2155151A GB714596A (en) 1951-09-13 1951-09-13 Improvements relating to ignition means for combustion chambers, particularly for use in gas turbine plant
FR1068816D FR1068816A (en) 1951-09-13 1952-09-04 Improvements to ignition devices for continuous combustion processes such as in gas turbine installations
CH308091D CH308091A (en) 1951-09-13 1952-09-11 Method for igniting the fuel in a gas turbine combustor.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2155151A GB714596A (en) 1951-09-13 1951-09-13 Improvements relating to ignition means for combustion chambers, particularly for use in gas turbine plant

Publications (1)

Publication Number Publication Date
GB714596A true GB714596A (en) 1954-09-01

Family

ID=10164799

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2155151A Expired GB714596A (en) 1951-09-13 1951-09-13 Improvements relating to ignition means for combustion chambers, particularly for use in gas turbine plant

Country Status (4)

Country Link
BE (1) BE513952A (en)
CH (1) CH308091A (en)
FR (1) FR1068816A (en)
GB (1) GB714596A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941363A (en) * 1955-04-11 1960-06-21 Bendix Aviat Corp Dual baffled igniter for combustion chamber

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2941363A (en) * 1955-04-11 1960-06-21 Bendix Aviat Corp Dual baffled igniter for combustion chamber

Also Published As

Publication number Publication date
BE513952A (en)
CH308091A (en) 1955-06-30
FR1068816A (en) 1954-07-01

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