IT956447B - COMBUSTION RING CHAMBER FOR GAS TURBINE ENGINES - Google Patents

COMBUSTION RING CHAMBER FOR GAS TURBINE ENGINES

Info

Publication number
IT956447B
IT956447B IT197225528A IT2552872A IT956447B IT 956447 B IT956447 B IT 956447B IT 197225528 A IT197225528 A IT 197225528A IT 2552872 A IT2552872 A IT 2552872A IT 956447 B IT956447 B IT 956447B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engines
ring chamber
combustion ring
combustion
Prior art date
Application number
IT197225528A
Other languages
Italian (it)
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
Application granted granted Critical
Publication of IT956447B publication Critical patent/IT956447B/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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
IT197225528A 1971-06-11 1972-06-10 COMBUSTION RING CHAMBER FOR GAS TURBINE ENGINES IT956447B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2747171 1971-06-11

Publications (1)

Publication Number Publication Date
IT956447B true IT956447B (en) 1973-10-10

Family

ID=10260136

Family Applications (1)

Application Number Title Priority Date Filing Date
IT197225528A IT956447B (en) 1971-06-11 1972-06-10 COMBUSTION RING CHAMBER FOR GAS TURBINE ENGINES

Country Status (4)

Country Link
US (1) US3797236A (en)
JP (1) JPS5334247B1 (en)
FR (1) FR2140625B1 (en)
IT (1) IT956447B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE375583B (en) * 1973-05-22 1975-04-21 United Turbine Ab & Co
US5031399A (en) * 1989-07-24 1991-07-16 Sundstrand Corporation Turbine including a thermal growth accommodating mount for a vane assembly
US5280703A (en) * 1989-12-11 1994-01-25 Sundstrand Corporation Turbine nozzle cooling
US7559203B2 (en) * 2005-09-16 2009-07-14 Pratt & Whitney Canada Corp. Cooled support boss for a combustor in a gas turbine engine
FR2920525B1 (en) * 2007-08-31 2014-06-13 Snecma SEPARATOR FOR SUPPLYING THE COOLING AIR OF A TURBINE
EP2428647B1 (en) * 2010-09-08 2018-07-11 Ansaldo Energia IP UK Limited Transitional Region for a Combustion Chamber of a Gas Turbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL69245C (en) * 1946-01-09
US2710523A (en) * 1951-09-27 1955-06-14 A V Roe Canada Ltd Gas turbine tail cone
US2924537A (en) * 1957-07-22 1960-02-09 Martin Co Laminated thermal insulation
US3092962A (en) * 1960-03-16 1963-06-11 Thiokol Chemical Corp Casings for rocket motors
US3229464A (en) * 1962-01-15 1966-01-18 Bendix Corp Combustor comprising a flame tube and insulating means
GB1059199A (en) * 1965-10-20 1967-02-15 Rolls Royce Flame tube

Also Published As

Publication number Publication date
FR2140625B1 (en) 1977-12-23
DE2227960A1 (en) 1973-01-04
DE2227960B2 (en) 1976-05-26
FR2140625A1 (en) 1973-01-19
US3797236A (en) 1974-03-19
JPS5334247B1 (en) 1978-09-19

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