IT8322399A0 - COMBUSTOR JACKET WITH DUAL-PURPOSE COOLING AIR FLOW. - Google Patents

COMBUSTOR JACKET WITH DUAL-PURPOSE COOLING AIR FLOW.

Info

Publication number
IT8322399A0
IT8322399A0 IT8322399A IT2239983A IT8322399A0 IT 8322399 A0 IT8322399 A0 IT 8322399A0 IT 8322399 A IT8322399 A IT 8322399A IT 2239983 A IT2239983 A IT 2239983A IT 8322399 A0 IT8322399 A0 IT 8322399A0
Authority
IT
Italy
Prior art keywords
dual
air flow
cooling air
purpose cooling
combustor jacket
Prior art date
Application number
IT8322399A
Other languages
Italian (it)
Other versions
IT1194584B (en
Inventor
Jacob Sherman Hoffman
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8322399A0 publication Critical patent/IT8322399A0/en
Application granted granted Critical
Publication of IT1194584B publication Critical patent/IT1194584B/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
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies
    • 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
IT22399/83A 1982-08-16 1983-08-03 DOUBLE FUNCTION COMBUSTER SHIRT WITH AIR FLOW IT1194584B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US40810482A 1982-08-16 1982-08-16

Publications (2)

Publication Number Publication Date
IT8322399A0 true IT8322399A0 (en) 1983-08-03
IT1194584B IT1194584B (en) 1988-09-22

Family

ID=23614881

Family Applications (1)

Application Number Title Priority Date Filing Date
IT22399/83A IT1194584B (en) 1982-08-16 1983-08-03 DOUBLE FUNCTION COMBUSTER SHIRT WITH AIR FLOW

Country Status (6)

Country Link
JP (1) JPS5969626A (en)
CA (1) CA1208922A (en)
DE (1) DE3328682A1 (en)
FR (1) FR2531748B1 (en)
GB (1) GB2125950B (en)
IT (1) IT1194584B (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0660740B2 (en) * 1985-04-05 1994-08-10 工業技術院長 Gas turbine combustor
US4984429A (en) * 1986-11-25 1991-01-15 General Electric Company Impingement cooled liner for dry low NOx venturi combustor
US5012645A (en) * 1987-08-03 1991-05-07 United Technologies Corporation Combustor liner construction for gas turbine engine
FR2668246B1 (en) * 1990-10-17 1994-12-09 Snecma COMBUSTION CHAMBER PROVIDED WITH A WALL COOLING DEVICE.
DE4244301C2 (en) * 1992-12-28 2001-09-13 Abb Research Ltd Impact cooling device
DE4444961A1 (en) * 1994-12-16 1996-06-20 Mtu Muenchen Gmbh Device for cooling in particular the rear wall of the flame tube of a combustion chamber for gas turbine engines
GB9505067D0 (en) * 1995-03-14 1995-05-03 Europ Gas Turbines Ltd Combustor and operating method for gas or liquid-fuelled turbine
DE19547703C2 (en) * 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Combustion chamber, in particular ring combustion chamber, for gas turbine engines
US7036316B2 (en) * 2003-10-17 2006-05-02 General Electric Company Methods and apparatus for cooling turbine engine combustor exit temperatures
US7051532B2 (en) * 2003-10-17 2006-05-30 General Electric Company Methods and apparatus for film cooling gas turbine engine combustors
US7270175B2 (en) * 2004-01-09 2007-09-18 United Technologies Corporation Extended impingement cooling device and method
GB0601413D0 (en) 2006-01-25 2006-03-08 Rolls Royce Plc Wall elements for gas turbine engine combustors
EP1813869A3 (en) 2006-01-25 2013-08-14 Rolls-Royce plc Wall elements for gas turbine engine combustors
GB0601418D0 (en) 2006-01-25 2006-03-08 Rolls Royce Plc Wall elements for gas turbine engine combustors
CN108167864A (en) * 2017-11-20 2018-06-15 北京动力机械研究所 Burner inner liner and high-pressure turbine guider integral structure
CN111648866A (en) * 2020-04-14 2020-09-11 南京航空航天大学 Impact air film-divergent hole composite cooling structure
US11859819B2 (en) 2021-10-15 2024-01-02 General Electric Company Ceramic composite combustor dome and liners

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB721209A (en) * 1951-09-24 1955-01-05 Power Jets Res & Dev Ltd Combustion apparatus
GB763692A (en) * 1955-01-07 1956-12-12 Svenska Turbinfab Ab Improved combustion chamber for gas turbines
GB845971A (en) * 1958-07-21 1960-08-24 Gen Electric Improvements relating to combustion chambers for gas turbine engines
US3777484A (en) * 1971-12-08 1973-12-11 Gen Electric Shrouded combustion liner
IL42390A0 (en) * 1972-08-02 1973-07-30 Gen Electric Impingement cooled combustor dome
DE2339366A1 (en) * 1972-08-15 1974-02-28 Stal Laval Turbin Ab COMBUSTION CHAMBER FOR GAS TURBINE
CA980584A (en) * 1972-11-10 1975-12-30 Edward E. Ekstedt Double walled impingement cooled combustor
FR2312654A1 (en) * 1975-05-28 1976-12-24 Snecma COMBUSTION CHAMBERS IMPROVEMENTS FOR GAS TURBINE ENGINES
GB2034874A (en) * 1978-11-03 1980-06-11 Gen Electric Gas turbine engine combustor
US4312186A (en) * 1979-10-17 1982-01-26 General Motors Corporation Shingled laminated porous material
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
GB2087065B (en) * 1980-11-08 1984-11-07 Rolls Royce Wall structure for a combustion chamber

Also Published As

Publication number Publication date
FR2531748B1 (en) 1987-08-28
GB2125950A (en) 1984-03-14
GB2125950B (en) 1986-09-24
GB8316374D0 (en) 1983-07-20
FR2531748A1 (en) 1984-02-17
DE3328682A1 (en) 1984-03-08
CA1208922A (en) 1986-08-05
IT1194584B (en) 1988-09-22
JPS5969626A (en) 1984-04-19

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