GB627722A - Improvements in or relating to gas-turbine-engines - Google Patents

Improvements in or relating to gas-turbine-engines

Info

Publication number
GB627722A
GB627722A GB3254946A GB3254946A GB627722A GB 627722 A GB627722 A GB 627722A GB 3254946 A GB3254946 A GB 3254946A GB 3254946 A GB3254946 A GB 3254946A GB 627722 A GB627722 A GB 627722A
Authority
GB
United Kingdom
Prior art keywords
igniter
engine
combustion
cartridges
cartridge
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
GB3254946A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB3254946A priority Critical patent/GB627722A/en
Publication of GB627722A publication Critical patent/GB627722A/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

627,722. Igniting burners. MARSDEN, J. R. Nov. 1, 1946, No. 32549. [Class 75(iii)] [Also in Group XXI] A gas turbine engine has mounted on it an igniter 15 for initiating combustion, the igniter comprising a breech mechanism formed with a chamber 18 to receive a cartridge 19 and with a passage 23 which, by communicating with the chamber 18 and with the combustion space of the engine, initiates combustion when the cartridge is discharged. In the construction shown a number of cartridges are carried by a cylindrical magazine 17 whose spindle 20 is held between a forked portion 21 of the igniter by a pin 22. The cartridges when in the operative position are in line with a contact 26 through which current is supplied for effecting discharge. The igniter has a flange 16 whereby it is secured to the air casing 10 around the flame tube 11 of the engine. The magazine may be rotated in any known manner to bring the chambers 18 successively in line with the discharge device. In a modification the firing mechanism comprises a solenoid-operated or a trigger-operated striker.
GB3254946A 1946-11-01 1946-11-01 Improvements in or relating to gas-turbine-engines Expired GB627722A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3254946A GB627722A (en) 1946-11-01 1946-11-01 Improvements in or relating to gas-turbine-engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3254946A GB627722A (en) 1946-11-01 1946-11-01 Improvements in or relating to gas-turbine-engines

Publications (1)

Publication Number Publication Date
GB627722A true GB627722A (en) 1949-08-15

Family

ID=10340314

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3254946A Expired GB627722A (en) 1946-11-01 1946-11-01 Improvements in or relating to gas-turbine-engines

Country Status (1)

Country Link
GB (1) GB627722A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE942237C (en) * 1952-02-20 1956-04-26 Plessey Co Ltd Device for feeding the combustion chamber of a gas turbine plant with liquid fuel
DE942549C (en) * 1953-06-02 1956-05-03 Plessey Co Ltd Device for the flow control and ignition of liquid fuel, in particular start-up device for gas turbine combustion chambers
US3084504A (en) * 1959-05-26 1963-04-09 Thompson Ramo Wooldridge Inc Rocket engine
US3124933A (en) * 1964-03-17 Leroy stram
US3261163A (en) * 1961-06-19 1966-07-19 Aerojet General Co Rocket motor testing apparatus
US3457726A (en) * 1966-07-26 1969-07-29 Thomson Houston Comp Francaise Incrementally controllable-thrust propulsion device
EP4019838A1 (en) * 2020-12-23 2022-06-29 Collins Engine Nozzles, Inc. Torch ignitors with tangential injection

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3124933A (en) * 1964-03-17 Leroy stram
DE942237C (en) * 1952-02-20 1956-04-26 Plessey Co Ltd Device for feeding the combustion chamber of a gas turbine plant with liquid fuel
DE942549C (en) * 1953-06-02 1956-05-03 Plessey Co Ltd Device for the flow control and ignition of liquid fuel, in particular start-up device for gas turbine combustion chambers
US3084504A (en) * 1959-05-26 1963-04-09 Thompson Ramo Wooldridge Inc Rocket engine
US3261163A (en) * 1961-06-19 1966-07-19 Aerojet General Co Rocket motor testing apparatus
US3457726A (en) * 1966-07-26 1969-07-29 Thomson Houston Comp Francaise Incrementally controllable-thrust propulsion device
EP4019838A1 (en) * 2020-12-23 2022-06-29 Collins Engine Nozzles, Inc. Torch ignitors with tangential injection
US11415058B2 (en) 2020-12-23 2022-08-16 Collins Engine Nozzles, Inc. Torch ignitors with tangential injection

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