CH500438A - Combustion chamber, in particular for gas turbine engines - Google Patents

Combustion chamber, in particular for gas turbine engines

Info

Publication number
CH500438A
CH500438A CH1530369A CH1530369A CH500438A CH 500438 A CH500438 A CH 500438A CH 1530369 A CH1530369 A CH 1530369A CH 1530369 A CH1530369 A CH 1530369A CH 500438 A CH500438 A CH 500438A
Authority
CH
Switzerland
Prior art keywords
combustion chamber
gas turbine
turbine engines
engines
combustion
Prior art date
Application number
CH1530369A
Other languages
German (de)
Inventor
John Faitani Joseph
Waclaw Jr Mieczkowski William
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of CH500438A publication Critical patent/CH500438A/en

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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
CH1530369A 1968-10-16 1969-10-13 Combustion chamber, in particular for gas turbine engines CH500438A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US76795368A 1968-10-16 1968-10-16

Publications (1)

Publication Number Publication Date
CH500438A true CH500438A (en) 1970-12-15

Family

ID=25081076

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1530369A CH500438A (en) 1968-10-16 1969-10-13 Combustion chamber, in particular for gas turbine engines

Country Status (9)

Country Link
US (1) US3498055A (en)
BE (1) BE740301A (en)
BR (1) BR6913369D0 (en)
CH (1) CH500438A (en)
DE (1) DE1951198C3 (en)
FR (1) FR2020807A1 (en)
GB (1) GB1252194A (en)
IL (1) IL33166A (en)
NL (1) NL6915585A (en)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1934700B2 (en) * 1969-07-09 1972-01-05 Mtu Muenchen Gmbh FUEL NOZZLE FOR GAS TURBINE ENGINES
US3630024A (en) * 1970-02-02 1971-12-28 Gen Electric Air swirler for gas turbine combustor
US3643430A (en) * 1970-03-04 1972-02-22 United Aircraft Corp Smoke reduction combustion chamber
USRE30160E (en) * 1970-03-04 1979-11-27 United Technologies Corporation Smoke reduction combustion chamber
US3656298A (en) * 1970-11-27 1972-04-18 Gen Motors Corp Combustion apparatus
US3741483A (en) * 1971-12-10 1973-06-26 Mitsubishi Heavy Ind Ltd Combustion air supply arrangement for gas turbines
US3916619A (en) * 1972-10-30 1975-11-04 Hitachi Ltd Burning method for gas turbine combustor and a construction thereof
JPS5342897B2 (en) * 1972-11-09 1978-11-15
GB1429677A (en) * 1973-03-20 1976-03-24 Rolls Royce Gas turbine engine combustion equipment
US3901446A (en) * 1974-05-09 1975-08-26 Us Air Force Induced vortex swirler
US4155220A (en) * 1977-01-21 1979-05-22 Westinghouse Electric Corp. Combustion apparatus for a gas turbine engine
US4151713A (en) * 1977-03-15 1979-05-01 United Technologies Corporation Burner for gas turbine engine
DE2919857C2 (en) * 1978-05-20 1982-09-02 Rolls-Royce Ltd., London Flame tube head with cooling ring for gas turbine combustion chambers
GB2099978A (en) * 1981-05-11 1982-12-15 Rolls Royce Gas turbine engine combustor
US5297385A (en) * 1988-05-31 1994-03-29 United Technologies Corporation Combustor
FR2673705A1 (en) * 1991-03-06 1992-09-11 Snecma Combustion chamber of a turbine engine equipped with an anti-coking device for the bottom of said chamber
AU2001232583A1 (en) 2000-02-14 2001-07-24 Potencia Medical Ag Hydraulic urinary incontinence treatment apparatus
DE102006041955A1 (en) * 2006-08-30 2008-03-20 Deutsches Zentrum für Luft- und Raumfahrt e.V. Method for controlling combustion in a combustion chamber and combustion chamber device
US9181812B1 (en) * 2009-05-05 2015-11-10 Majed Toqan Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines
US9027350B2 (en) * 2009-12-30 2015-05-12 Rolls-Royce Corporation Gas turbine engine having dome panel assembly with bifurcated swirler flow
US9599343B2 (en) * 2012-11-28 2017-03-21 General Electric Company Fuel nozzle for use in a turbine engine and method of assembly
US9228747B2 (en) * 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
USD911402S1 (en) * 2019-07-18 2021-02-23 Illinois Tool Works Inc. Chamber
US11885497B2 (en) * 2019-07-19 2024-01-30 Pratt & Whitney Canada Corp. Fuel nozzle with slot for cooling
US11933498B2 (en) 2020-10-13 2024-03-19 Venture Aerospace, Llc Aerospace structure methods of manufacturing

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2560207A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Annular combustion chamber with circumferentially spaced double air-swirl burners
US2700416A (en) * 1949-06-30 1955-01-25 Rolls Royce Fuel injection means for gas-turbine engines and combustion equipment used therewith
US2982099A (en) * 1956-10-09 1961-05-02 Rolls Royce Fuel injection arrangement in combustion equipment for gas turbine engines
US3134229A (en) * 1961-10-02 1964-05-26 Gen Electric Combustion chamber

Also Published As

Publication number Publication date
FR2020807A1 (en) 1970-07-17
BE740301A (en) 1970-03-16
DE1951198A1 (en) 1970-05-14
BR6913369D0 (en) 1973-06-26
GB1252194A (en) 1971-11-03
IL33166A0 (en) 1970-03-22
US3498055A (en) 1970-03-03
DE1951198C3 (en) 1973-12-06
DE1951198B2 (en) 1973-05-17
NL6915585A (en) 1970-04-20
IL33166A (en) 1973-08-29

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Legal Events

Date Code Title Description
PL Patent ceased