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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
BE514534D 1951-05-31 BE514534A (en:Method)

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:Method)

Family

ID=22859732

Family Applications (1)

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

Country Status (7)

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

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 (fr) * 1964-09-16 1965-12-17 Perfectionnement apporté aux chambres de combustion
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 (ja) * 1982-10-06 1984-04-16 Hitachi Ltd ガスタ−ビン燃焼器
US5323605A (en) * 1990-10-01 1994-06-28 General Electric Company Double dome arched combustor
FR2668246B1 (fr) * 1990-10-17 1994-12-09 Snecma Chambre de combustion munie d'un dispositif de refroidissement de sa paroi.
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 (de) * 2002-04-02 2003-10-16 Rolls Royce Deutschland Brennkammer einer Gasturbine mit Starterfilmkühlung
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
EP3039340B1 (en) * 2013-08-30 2018-11-28 United Technologies Corporation Vena contracta swirling dilution passages for gas turbine engine combustor
US10443848B2 (en) * 2014-04-02 2019-10-15 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 (de) * 1935-07-17 1941-08-07 Rene Alexandre Arthur Couzinet Speiseeinrichtung fuer Gasturbinen
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:Method) * 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 (de) * 1947-06-23 1951-05-04 Armstrong Siddeley Motors Ltd Brennkammer fuer Brennkraftturbeinen
NL72524C (en:Method) * 1947-11-03
NL80817C (en:Method) * 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
NL79375C (en:Method)
GB731054A (en) 1955-06-01
US2742762A (en) 1956-04-24
DE935287C (de) 1955-11-17
CH317633A (fr) 1956-11-30
FR1065482A (fr) 1954-05-26

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