EG22526A - Combustion chamber for gas turbine - Google Patents

Combustion chamber for gas turbine

Info

Publication number
EG22526A
EG22526A EG20000714A EG20000714A EG22526A EG 22526 A EG22526 A EG 22526A EG 20000714 A EG20000714 A EG 20000714A EG 20000714 A EG20000714 A EG 20000714A EG 22526 A EG22526 A EG 22526A
Authority
EG
Egypt
Prior art keywords
combustion chamber
gas turbine
turbine
gas
combustion
Prior art date
Application number
EG20000714A
Other languages
English (en)
Inventor
Anthony Dean
Original Assignee
Nuovo Pignone Spa
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 Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Application granted granted Critical
Publication of EG22526A publication Critical patent/EG22526A/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
    • F23R3/002—Wall structures
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Spray-Type Burners (AREA)
EG20000714A 1999-05-31 2000-05-31 Combustion chamber for gas turbine EG22526A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT1999MI001207A ITMI991207A1 (it) 1999-05-31 1999-05-31 Camera di combustione per turbine a gas

Publications (1)

Publication Number Publication Date
EG22526A true EG22526A (en) 2003-03-31

Family

ID=11383082

Family Applications (1)

Application Number Title Priority Date Filing Date
EG20000714A EG22526A (en) 1999-05-31 2000-05-31 Combustion chamber for gas turbine

Country Status (12)

Country Link
US (1) US6434926B1 (xx)
EP (1) EP1058061B1 (xx)
AR (1) AR024167A1 (xx)
BR (1) BR0002176A (xx)
DE (1) DE60028127T2 (xx)
DZ (1) DZ3086A1 (xx)
EG (1) EG22526A (xx)
ES (1) ES2263434T3 (xx)
IT (1) ITMI991207A1 (xx)
MX (1) MXPA00005374A (xx)
NO (1) NO331223B1 (xx)
RU (1) RU2227874C2 (xx)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7121095B2 (en) * 2003-08-11 2006-10-17 General Electric Company Combustor dome assembly of a gas turbine engine having improved deflector plates
US20050241316A1 (en) * 2004-04-28 2005-11-03 Honeywell International Inc. Uniform effusion cooling method for a can combustion chamber
FR2889732B1 (fr) * 2005-08-12 2011-09-23 Snecma Chambre de combustion a tenue thermique amelioree
EP1767855A1 (de) * 2005-09-27 2007-03-28 Siemens Aktiengesellschaft Brennkammer und Gasturbinenanlage
EP2039999A1 (en) * 2007-09-24 2009-03-25 Siemens Aktiengesellschaft Combustion chamber
US20090090110A1 (en) * 2007-10-04 2009-04-09 Honeywell International, Inc. Faceted dome assemblies for gas turbine engine combustors
JP5537895B2 (ja) * 2009-10-21 2014-07-02 川崎重工業株式会社 ガスタービン燃焼器
GB201107095D0 (en) * 2011-04-28 2011-06-08 Rolls Royce Plc A head part of an annular combustion chamber
EP3084303B1 (en) * 2013-12-19 2022-01-26 Raytheon Technologies Corporation Thermal mechanical dimple array for a combustor wall assembly
US9625152B2 (en) * 2014-06-03 2017-04-18 Pratt & Whitney Canada Corp. Combustor heat shield for a gas turbine engine
JP7191723B2 (ja) * 2019-02-27 2022-12-19 三菱重工業株式会社 ガスタービン燃焼器及びガスタービン
US11525577B2 (en) 2020-04-27 2022-12-13 Raytheon Technologies Corporation Extended bulkhead panel

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4567730A (en) * 1983-10-03 1986-02-04 General Electric Company Shielded combustor
US5012645A (en) 1987-08-03 1991-05-07 United Technologies Corporation Combustor liner construction for gas turbine engine
US4843825A (en) * 1988-05-16 1989-07-04 United Technologies Corporation Combustor dome heat shield
US5480162A (en) * 1993-09-08 1996-01-02 United Technologies Corporation Axial load carrying brush seal
US5657633A (en) * 1995-12-29 1997-08-19 General Electric Company Centerbody for a multiple annular combustor

Also Published As

Publication number Publication date
NO20002766D0 (no) 2000-05-30
DE60028127T2 (de) 2006-12-14
NO331223B1 (no) 2011-11-07
ITMI991207A1 (it) 2000-12-01
DE60028127D1 (de) 2006-06-29
BR0002176A (pt) 2001-01-02
EP1058061A1 (en) 2000-12-06
RU2227874C2 (ru) 2004-04-27
MXPA00005374A (es) 2002-04-24
ITMI991207A0 (it) 1999-05-31
US6434926B1 (en) 2002-08-20
ES2263434T3 (es) 2006-12-16
AR024167A1 (es) 2002-09-04
DZ3086A1 (fr) 2004-06-20
NO20002766L (no) 2000-12-01
EP1058061B1 (en) 2006-05-24

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