BE514534A - - Google Patents

Info

Publication number
BE514534A
BE514534A BE514534DA BE514534A BE 514534 A BE514534 A BE 514534A BE 514534D A BE514534D A BE 514534DA BE 514534 A BE514534 A BE 514534A
Authority
BE
Belgium
Application number
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.)
Publication of BE514534A publication Critical patent/BE514534A/xx

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
BE514534D 1951-05-31 BE514534A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US229071A US2742762A (en) 1951-05-31 1951-05-31 Combustion chamber for axial flow gas turbines

Publications (1)

Publication Number Publication Date
BE514534A true BE514534A (en)

Family

ID=22859732

Family Applications (1)

Application Number Title Priority Date Filing Date
BE514534D BE514534A (en) 1951-05-31

Country Status (7)

Country Link
US (1) US2742762A (en)
BE (1) BE514534A (en)
CH (1) CH317633A (en)
DE (1) DE935287C (en)
FR (1) FR1065482A (en)
GB (1) GB731054A (en)
NL (1) NL79375C (en)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2890569A (en) * 1954-05-03 1959-06-16 Phillips Petroleum Co Removal of carbon deposits in jet engines
US2902823A (en) * 1956-11-21 1959-09-08 Clarence E Wagner Design for a stainless steel or aluminum gas generator wall spraying system for combustion chamber
US3210935A (en) * 1959-09-23 1965-10-12 Lyman C Fisher Jetevator for missile control
FR1421372A (en) * 1964-09-16 1965-12-17 Improvements to combustion chambers
US3874169A (en) * 1971-01-14 1975-04-01 Stal Laval Turbin Ab Combustion chamber for gas turbines
US3981142A (en) * 1974-04-01 1976-09-21 General Motors Corporation Ceramic combustion liner
US4298338A (en) * 1976-12-30 1981-11-03 Owens-Illinois, Inc. Liquid fuel burners
JPS5966619A (en) * 1982-10-06 1984-04-16 Hitachi Ltd Gas turbine combustor
US5323605A (en) * 1990-10-01 1994-06-28 General Electric Company Double dome arched combustor
FR2668246B1 (en) * 1990-10-17 1994-12-09 Snecma COMBUSTION CHAMBER PROVIDED WITH A WALL COOLING DEVICE.
CA2089272C (en) * 1992-03-23 2002-09-03 James Norman Reinhold, Jr. Impact resistant combustor
US5755093A (en) * 1995-05-01 1998-05-26 United Technologies Corporation Forced air cooled gas turbine exhaust liner
DE10214573A1 (en) * 2002-04-02 2003-10-16 Rolls Royce Deutschland Combustion chamber of a gas turbine with starter film cooling
US20050241316A1 (en) * 2004-04-28 2005-11-03 Honeywell International Inc. Uniform effusion cooling method for a can combustion chamber
US8281600B2 (en) * 2007-01-09 2012-10-09 General Electric Company Thimble, sleeve, and method for cooling a combustor assembly
US20100037622A1 (en) * 2008-08-18 2010-02-18 General Electric Company Contoured Impingement Sleeve Holes
US8161752B2 (en) * 2008-11-20 2012-04-24 Honeywell International Inc. Combustors with inserts between dual wall liners
GB201116608D0 (en) * 2011-09-27 2011-11-09 Rolls Royce Plc A method of operating a combustion chamber
US9328923B2 (en) * 2012-10-10 2016-05-03 General Electric Company System and method for separating fluids
US20160201908A1 (en) * 2013-08-30 2016-07-14 United Technologies Corporation Vena contracta swirling dilution passages for gas turbine engine combustor
EP2927595B1 (en) * 2014-04-02 2019-11-13 United Technologies Corporation Grommet assembly and method of design
US20160047549A1 (en) * 2014-08-15 2016-02-18 Rolls-Royce Corporation Ceramic matrix composite components with inserts

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE709065C (en) * 1935-07-17 1941-08-07 Rene Alexandre Arthur Couzinet Feeding device for gas turbines
US2227666A (en) * 1936-12-10 1941-01-07 Bbc Brown Boveri & Cie Starting up system for heat producing and consuming plants
US2471101A (en) * 1945-03-31 1949-05-24 Charles E Feinberg Secondary combustion air distribution control for bridge wall furnaces
GB603485A (en) * 1946-02-23 1948-06-16 Armstrong Siddeley Motors Ltd Liquid fuel combustion chamber
FR962862A (en) * 1946-10-26 1950-06-22
US2601390A (en) * 1946-11-07 1952-06-24 Westinghouse Electric Corp Combustion chamber for gas turbines with circumferentially arranged pulverized solidfuel and air nozzles
DE804982C (en) * 1947-06-23 1951-05-04 Armstrong Siddeley Motors Ltd Combustion chamber for internal combustion turbine legs
BE485523A (en) * 1947-11-03
NL80817C (en) * 1947-11-03
US2631429A (en) * 1948-06-08 1953-03-17 Jr Harold M Jacklin Cooling arrangement for radial flow gas turbines having coaxial combustors
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner

Also Published As

Publication number Publication date
GB731054A (en) 1955-06-01
DE935287C (en) 1955-11-17
NL79375C (en)
CH317633A (en) 1956-11-30
US2742762A (en) 1956-04-24
FR1065482A (en) 1954-05-26

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