GB660775A - An improved combustion and ignition apparatus for a gas turbine engine - Google Patents

An improved combustion and ignition apparatus for a gas turbine engine

Info

Publication number
GB660775A
GB660775A GB32183/49A GB3218349A GB660775A GB 660775 A GB660775 A GB 660775A GB 32183/49 A GB32183/49 A GB 32183/49A GB 3218349 A GB3218349 A GB 3218349A GB 660775 A GB660775 A GB 660775A
Authority
GB
United Kingdom
Prior art keywords
jet
igniter
combustion
gas turbine
turbine engine
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
GB32183/49A
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.)
FREDERICK DENISON MORGAN WILLI
Original Assignee
FREDERICK DENISON MORGAN WILLI
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 FREDERICK DENISON MORGAN WILLI filed Critical FREDERICK DENISON MORGAN WILLI
Publication of GB660775A publication Critical patent/GB660775A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
    • 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
    • F02C7/266—Electric

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

660,775. Lighting vapour burners. WILLIAMS, F. D. M. Dec. 15, 1949 [Dec. 24, 1948], No. 32183/49. Classes 75(i) and 75(iii) Combustion and ignition apparatus for a gas turbine engine comprises a fuel injector head 9, Fig. 1, located at the upstream end of a flame tube 6, and including an igniter jet 11, Fig. 3, whereby an igniting flame may be directed substantially along the longitudinal axis of the flame tube 6 and applied to longitudinally extending vaporizing tubes 7, each having an inlet exposed to the air stream through the combustion chamber and an outlet end discharging into the flame tube 6, an igniter 13 situated in front of the jet 11, and a plurality of fuel supply jets 10 arranged around the jet 11 and directed into the inlet ends of the vaporizing tubes 7. The jet 11 is of an atomizing type and is supplied with fuel through a pipe 16 extending coaxially through a pipe 18 which supplies the jets 10. The igniter comprises a sparking electrode 12 mounted directly on the head 9 and a sparking electrode 13 connected by a high-tension lead through a tube 14 to a terminal mounted outside the combustion chamber.. When combustion has been established the current to the igniter is switched off and the fuel supply to the igniter jet 11 is discontinued.
GB32183/49A 1948-12-24 1949-12-15 An improved combustion and ignition apparatus for a gas turbine engine Expired GB660775A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US67118A US2541900A (en) 1948-12-24 1948-12-24 Multiple fuel jet burner and torch igniter unit with fuel vaporizing tubes

Publications (1)

Publication Number Publication Date
GB660775A true GB660775A (en) 1951-11-14

Family

ID=22073825

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32183/49A Expired GB660775A (en) 1948-12-24 1949-12-15 An improved combustion and ignition apparatus for a gas turbine engine

Country Status (4)

Country Link
US (1) US2541900A (en)
DE (1) DE804504C (en)
FR (1) FR1006966A (en)
GB (1) GB660775A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1015271B (en) * 1955-04-05 1957-09-05 Armstrong Siddeley Motors Ltd Main combustion chamber for gas turbines with ignition chamber
US5761906A (en) * 1995-01-13 1998-06-09 European Gas Turbines Limited Fuel injector swirler arrangement having a shield means for creating fuel rich pockets in gas-or liquid-fuelled turbine

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2735633A (en) * 1956-02-21 Jet propelled aircraft
US3273621A (en) * 1966-09-20 Burner assembly
US2646664A (en) * 1949-02-24 1953-07-28 A V Roe Canada Ltd Annular fuel vaporizer for gas turbine engines
US2706889A (en) * 1949-08-18 1955-04-26 Armstrong Siddeley Motors Ltd Combustion chambers of gas turbine engines
US2678535A (en) * 1950-04-12 1954-05-18 A V Roe Canada Ltd Liquid fuel injecting burner
US2655786A (en) * 1950-09-18 1953-10-20 Phillips Petroleum Co Method of operating jet engines with fuel reforming
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
US2781637A (en) * 1950-12-15 1957-02-19 Gen Motors Corp Combustion chamber with fuel vaporizer
US2674846A (en) * 1950-12-18 1954-04-13 Lummus Co Combustion chamber with baffle means to control secondary air
US2648197A (en) * 1951-01-06 1953-08-11 A V Roe Canada Ltd Vaporizer tube system
US2828605A (en) * 1951-03-19 1958-04-01 Power Jets Res & Dev Ltd Method of generating combustion gases by burning a gaseous combustible mixture
US2693676A (en) * 1951-06-11 1954-11-09 Westinghouse Electric Corp Combustion apparatus with multipleoutlet fuel vaporizing tubes
US2805547A (en) * 1952-02-01 1957-09-10 Sherry Peter Temperature responsive control for fuel and water vaporizers in combustion chamber
US2727358A (en) * 1952-03-27 1955-12-20 A V Roe Canada Ltd Reverse-flow vaporizer with single inlet and plural outlets
US2982098A (en) * 1953-04-22 1961-05-02 Power Jets Res & Dev Ltd Liquid fuel vaporizing combustion systems
GB798474A (en) * 1955-03-16 1958-07-23 Bristol Aero Engines Ltd Improvements in or relating to combustion chambers
US2941364A (en) * 1955-04-05 1960-06-21 Armstrong Siddeley Motors Ltd Igniter chamber for a gas turbine engine
US3018626A (en) * 1960-02-02 1962-01-30 Gen Electric Vapor combustion system
US3287913A (en) * 1962-07-09 1966-11-29 Aerojet General Co Igniter
US3398528A (en) * 1965-10-05 1968-08-27 Ishikawajima Harima Heavy Ind Evaporation type burner
US3548592A (en) * 1969-06-13 1970-12-22 Gen Electric Combination fuel nozzle and spark plug for a gas turbine
GB1429677A (en) * 1973-03-20 1976-03-24 Rolls Royce Gas turbine engine combustion equipment
US5127822A (en) * 1987-08-14 1992-07-07 Toa Nenryo Kogyo Kabushiki Kaisha Combustion apparatus with atomizer and method of controlling same
US5163287A (en) * 1989-12-22 1992-11-17 Sundstrand Corporation Stored energy combustor with fuel injector containing igniter means for accommodating thermal expansion
CN103343984B (en) * 2013-06-24 2016-01-06 北京航空航天大学 A kind of burner for living beings replacing fuel oil combustion test
US11473505B2 (en) 2020-11-04 2022-10-18 Delavan Inc. Torch igniter cooling system
US11692488B2 (en) 2020-11-04 2023-07-04 Delavan Inc. Torch igniter cooling system
US11608783B2 (en) 2020-11-04 2023-03-21 Delavan, Inc. Surface igniter cooling system
US11635027B2 (en) 2020-11-18 2023-04-25 Collins Engine Nozzles, Inc. Fuel systems for torch ignition devices
US11421602B2 (en) 2020-12-16 2022-08-23 Delavan Inc. Continuous ignition device exhaust manifold
US11226103B1 (en) 2020-12-16 2022-01-18 Delavan Inc. High-pressure continuous ignition device
US11635210B2 (en) 2020-12-17 2023-04-25 Collins Engine Nozzles, Inc. Conformal and flexible woven heat shields for gas turbine engine components
US11754289B2 (en) 2020-12-17 2023-09-12 Delavan, Inc. Axially oriented internally mounted continuous ignition device: removable nozzle
US11486309B2 (en) 2020-12-17 2022-11-01 Delavan Inc. Axially oriented internally mounted continuous ignition device: removable hot surface igniter
US11209164B1 (en) 2020-12-18 2021-12-28 Delavan Inc. Fuel injector systems for torch igniters
US11680528B2 (en) 2020-12-18 2023-06-20 Delavan Inc. Internally-mounted torch igniters with removable igniter heads
US11286862B1 (en) 2020-12-18 2022-03-29 Delavan Inc. Torch injector systems for gas turbine combustors
CN112963273B (en) * 2021-03-03 2022-07-01 中国人民解放军空军工程大学 Self-air-entraining kerosene pre-combustion cracking activation device and method for concave cavity flame stabilizer
CN114234237B (en) * 2021-12-20 2023-03-31 中国人民解放军总参谋部第六十研究所 Head preparation method for wide-envelope starting of evaporating tube combustion chamber

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL82403C (en) * 1939-12-09
GB603485A (en) * 1946-02-23 1948-06-16 Armstrong Siddeley Motors Ltd Liquid fuel combustion chamber

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1015271B (en) * 1955-04-05 1957-09-05 Armstrong Siddeley Motors Ltd Main combustion chamber for gas turbines with ignition chamber
US5761906A (en) * 1995-01-13 1998-06-09 European Gas Turbines Limited Fuel injector swirler arrangement having a shield means for creating fuel rich pockets in gas-or liquid-fuelled turbine

Also Published As

Publication number Publication date
US2541900A (en) 1951-02-13
DE804504C (en) 1951-04-23
FR1006966A (en) 1952-04-29

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