BE849124A - Chambre de combustion perfectionnee - Google Patents

Chambre de combustion perfectionnee

Info

Publication number
BE849124A
BE849124A BE173015A BE173015A BE849124A BE 849124 A BE849124 A BE 849124A BE 173015 A BE173015 A BE 173015A BE 173015 A BE173015 A BE 173015A BE 849124 A BE849124 A BE 849124A
Authority
BE
Belgium
Prior art keywords
perfected
combustion chamber
combustion
chamber
perfected combustion
Prior art date
Application number
BE173015A
Other languages
English (en)
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 BE849124A publication Critical patent/BE849124A/fr

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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
BE173015A 1975-12-11 1976-12-07 Chambre de combustion perfectionnee BE849124A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/639,617 US3990232A (en) 1975-12-11 1975-12-11 Combustor dome assembly having improved cooling means

Publications (1)

Publication Number Publication Date
BE849124A true BE849124A (fr) 1977-04-01

Family

ID=24564859

Family Applications (1)

Application Number Title Priority Date Filing Date
BE173015A BE849124A (fr) 1975-12-11 1976-12-07 Chambre de combustion perfectionnee

Country Status (5)

Country Link
US (1) US3990232A (fr)
BE (1) BE849124A (fr)
DE (1) DE2655722A1 (fr)
FR (1) FR2334824A1 (fr)
IT (1) IT1065534B (fr)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
US4195476A (en) * 1978-04-27 1980-04-01 General Motors Corporation Combustor construction
US4222230A (en) * 1978-08-14 1980-09-16 General Electric Company Combustor dome assembly
JPS5619340U (fr) * 1979-07-25 1981-02-20
US4852355A (en) * 1980-12-22 1989-08-01 General Electric Company Dispensing arrangement for pressurized air
US4584834A (en) * 1982-07-06 1986-04-29 General Electric Company Gas turbine engine carburetor
US5012645A (en) * 1987-08-03 1991-05-07 United Technologies Corporation Combustor liner construction for gas turbine engine
US5142871A (en) * 1991-01-22 1992-09-01 General Electric Company Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures
US5181377A (en) * 1991-04-16 1993-01-26 General Electric Company Damped combustor cowl structure
CA2070518C (fr) * 1991-07-01 2001-10-02 Adrian Mark Ablett Ensemble dome pour chambre de combustion
JP2597800B2 (ja) * 1992-06-12 1997-04-09 ゼネラル・エレクトリック・カンパニイ ガスタービンエンジン用燃焼器
US5363654A (en) * 1993-05-10 1994-11-15 General Electric Company Recuperative impingement cooling of jet engine components
US5924288A (en) * 1994-12-22 1999-07-20 General Electric Company One-piece combustor cowl
US5680767A (en) * 1995-09-11 1997-10-28 General Electric Company Regenerative combustor cooling in a gas turbine engine
US6725667B2 (en) 2002-08-22 2004-04-27 General Electric Company Combustor dome for gas turbine engine
US7246494B2 (en) * 2004-09-29 2007-07-24 General Electric Company Methods and apparatus for fabricating gas turbine engine combustors
US7360364B2 (en) * 2004-12-17 2008-04-22 General Electric Company Method and apparatus for assembling gas turbine engine combustors
FR2905166B1 (fr) * 2006-08-28 2008-11-14 Snecma Sa Chambre de combustion annulaire d'une turbomachine.
US7975487B2 (en) * 2006-09-21 2011-07-12 Solar Turbines Inc. Combustor assembly for gas turbine engine
FR2943404B1 (fr) * 2009-03-20 2015-08-07 Snecma Fond de chambre de combustion definissant en partie une fente pour le passage d'un film d'air de refroissement
US10598380B2 (en) * 2017-09-21 2020-03-24 General Electric Company Canted combustor for gas turbine engine
US11859819B2 (en) 2021-10-15 2024-01-02 General Electric Company Ceramic composite combustor dome and liners

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2709338A (en) * 1953-01-16 1955-05-31 Rolls Royce Double-walled ducting for conveying hot gas with means to interconnect the walls
GB791753A (en) * 1955-02-23 1958-03-12 Bristol Aero Engines Ltd Improvements in or relating to flame tubes for use in combustion systems of gas turbine engines
GB851506A (en) * 1958-02-10 1960-10-19 Lucas Industries Ltd Liquid fuel combustion apparatus
US3134229A (en) * 1961-10-02 1964-05-26 Gen Electric Combustion chamber
US3385055A (en) * 1966-11-23 1968-05-28 United Aircraft Corp Combustion chamber with floating swirler rings
US3656298A (en) * 1970-11-27 1972-04-18 Gen Motors Corp Combustion apparatus
IL42390A0 (en) * 1972-08-02 1973-07-30 Gen Electric Impingement cooled combustor dome
US3854285A (en) * 1973-02-26 1974-12-17 Gen Electric Combustor dome assembly

Also Published As

Publication number Publication date
DE2655722C2 (fr) 1987-01-29
IT1065534B (it) 1985-02-25
FR2334824A1 (fr) 1977-07-08
US3990232A (en) 1976-11-09
FR2334824B1 (fr) 1980-08-29
DE2655722A1 (de) 1977-06-16

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: GENERAL ELECTRIC CY

Effective date: 19931231