CN1609427B - 膜式冷却燃气轮机燃烧器的方法和装置 - Google Patents

膜式冷却燃气轮机燃烧器的方法和装置 Download PDF

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Publication number
CN1609427B
CN1609427B CN2004100577513A CN200410057751A CN1609427B CN 1609427 B CN1609427 B CN 1609427B CN 2004100577513 A CN2004100577513 A CN 2004100577513A CN 200410057751 A CN200410057751 A CN 200410057751A CN 1609427 B CN1609427 B CN 1609427B
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CN
China
Prior art keywords
cooling
liner
film cooling
combustion chamber
gas turbine
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CN2004100577513A
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English (en)
Chinese (zh)
Other versions
CN1609427A (zh
Inventor
S·J·霍维尔
J·C·雅各布森
T·P·麦卡弗里
B·F·巴恩斯
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General Electric Co
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN1609427A publication Critical patent/CN1609427A/zh
Application granted granted Critical
Publication of CN1609427B publication Critical patent/CN1609427B/zh
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    • 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
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L15/00—Heating of air supplied for combustion
    • F23L15/04—Arrangements of recuperators
    • 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
    • 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
    • F23R2900/00017—Assembling combustion chamber liners or subparts
    • 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
    • F23R2900/03042—Film cooled combustion chamber walls or domes
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Spray-Type Burners (AREA)
CN2004100577513A 2003-10-17 2004-08-17 膜式冷却燃气轮机燃烧器的方法和装置 Expired - Fee Related CN1609427B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/688526 2003-10-17
US10/688,526 US7051532B2 (en) 2003-10-17 2003-10-17 Methods and apparatus for film cooling gas turbine engine combustors

Publications (2)

Publication Number Publication Date
CN1609427A CN1609427A (zh) 2005-04-27
CN1609427B true CN1609427B (zh) 2011-12-28

Family

ID=34377677

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2004100577513A Expired - Fee Related CN1609427B (zh) 2003-10-17 2004-08-17 膜式冷却燃气轮机燃烧器的方法和装置

Country Status (5)

Country Link
US (1) US7051532B2 (https=)
EP (1) EP1524472A3 (https=)
JP (1) JP4569952B2 (https=)
CN (1) CN1609427B (https=)
BR (1) BRPI0403055A (https=)

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US7093419B2 (en) * 2003-07-02 2006-08-22 General Electric Company Methods and apparatus for operating gas turbine engine combustors
US7464554B2 (en) * 2004-09-09 2008-12-16 United Technologies Corporation Gas turbine combustor heat shield panel or exhaust panel including a cooling device
FR2889732B1 (fr) * 2005-08-12 2011-09-23 Snecma Chambre de combustion a tenue thermique amelioree
US7716931B2 (en) * 2006-03-01 2010-05-18 General Electric Company Method and apparatus for assembling gas turbine engine
EP1832812A3 (de) * 2006-03-10 2012-01-04 Rolls-Royce Deutschland Ltd & Co KG Gasturbinenbrennkammerwand mit Dämpfung von Brennkammerschwingungen
FR2909748B1 (fr) * 2006-12-07 2009-07-10 Snecma Sa Fond de chambre, procede de realisation de celui-ci, chambre de combustion le comportant et turboreacteur en etant equipe
US8096133B2 (en) * 2008-05-13 2012-01-17 General Electric Company Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface
US20100223931A1 (en) * 2009-03-04 2010-09-09 General Electric Company Pattern cooled combustor liner
US8052378B2 (en) * 2009-03-18 2011-11-08 General Electric Company Film-cooling augmentation device and turbine airfoil incorporating the same
US20100239409A1 (en) * 2009-03-18 2010-09-23 General Electric Company Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil
FR2951245B1 (fr) * 2009-10-13 2013-05-17 Snecma Dispositif d'injection multi-point pour une chambre de combustion de turbomachine
US8429916B2 (en) * 2009-11-23 2013-04-30 Honeywell International Inc. Dual walled combustors with improved liner seals
US9027350B2 (en) * 2009-12-30 2015-05-12 Rolls-Royce Corporation Gas turbine engine having dome panel assembly with bifurcated swirler flow
US20120297784A1 (en) * 2011-05-24 2012-11-29 General Electric Company System and method for flow control in gas turbine engine
US8904802B2 (en) * 2011-06-30 2014-12-09 General Electric Company Turbomachine combustor assembly including a vortex modification system
US9964307B2 (en) 2012-09-30 2018-05-08 United Technologies Corporation Interface heat shield for a combustor of a gas turbine engine
US10072845B2 (en) 2012-11-15 2018-09-11 General Electric Company Fuel nozzle heat shield
US10260748B2 (en) * 2012-12-21 2019-04-16 United Technologies Corporation Gas turbine engine combustor with tailored temperature profile
EP3401529A1 (en) * 2013-03-14 2018-11-14 United Technologies Corporation Hollow-wall heat shield for fuel injector component
US10041675B2 (en) 2014-06-04 2018-08-07 Pratt & Whitney Canada Corp. Multiple ventilated rails for sealing of combustor heat shields
US9534785B2 (en) * 2014-08-26 2017-01-03 Pratt & Whitney Canada Corp. Heat shield labyrinth seal
US10132498B2 (en) * 2015-01-20 2018-11-20 United Technologies Corporation Thermal barrier coating of a combustor dilution hole
US10428736B2 (en) * 2016-02-25 2019-10-01 General Electric Company Combustor assembly
US10378771B2 (en) 2016-02-25 2019-08-13 General Electric Company Combustor assembly
FR3061761B1 (fr) * 2017-01-10 2021-01-01 Safran Aircraft Engines Chambre de combustion pour turbomachine
US10823416B2 (en) * 2017-08-10 2020-11-03 General Electric Company Purge cooling structure for combustor assembly
DE102018212394B4 (de) * 2018-07-25 2024-03-28 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerbaugruppe mit Strömungsleiteinrichtung aufweisendem Wandelement
CN111503660B (zh) * 2020-04-29 2021-07-16 中国航发湖南动力机械研究所 排气弯管和回流燃烧室
CN112484077B (zh) * 2020-11-25 2022-04-01 中国科学院工程热物理研究所 一种火焰筒头部的高效冷却结构

Citations (4)

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GB2125950A (en) * 1982-08-16 1984-03-14 Gen Electric Gas turbine combustor
US4567730A (en) * 1983-10-03 1986-02-04 General Electric Company Shielded combustor
US5353587A (en) * 1992-06-12 1994-10-11 General Electric Company Film cooling starter geometry for combustor lines
EP1096205A1 (en) * 1999-11-01 2001-05-02 General Electric Company Offset dilution combustion liner

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US4365470A (en) * 1980-04-02 1982-12-28 United Technologies Corporation Fuel nozzle guide and seal for a gas turbine engine
US4485630A (en) * 1982-12-08 1984-12-04 General Electric Company Combustor liner
JPH0648092B2 (ja) * 1985-04-04 1994-06-22 ゼネラル・エレクトリツク・カンパニイ 燃焼室構造
FR2639095B1 (fr) * 1988-11-17 1990-12-21 Snecma Chambre de combustion de turbomachine a bols de prevaporisation montes flottants
US4950129A (en) 1989-02-21 1990-08-21 General Electric Company Variable inlet guide vanes for an axial flow compressor
US5281085A (en) 1990-12-21 1994-01-25 General Electric Company Clearance control system for separately expanding or contracting individual portions of an annular shroud
US5228828A (en) 1991-02-15 1993-07-20 General Electric Company Gas turbine engine clearance control apparatus
US5222360A (en) 1991-10-30 1993-06-29 General Electric Company Apparatus for removably attaching a core frame to a vane frame with a stable mid ring
CA2070518C (en) * 1991-07-01 2001-10-02 Adrian Mark Ablett Combustor dome assembly
US5273396A (en) 1992-06-22 1993-12-28 General Electric Company Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud
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US6045325A (en) 1997-12-18 2000-04-04 United Technologies Corporation Apparatus for minimizing inlet airflow turbulence in a gas turbine engine
US6543233B2 (en) * 2001-02-09 2003-04-08 General Electric Company Slot cooled combustor liner
US7007481B2 (en) * 2003-09-10 2006-03-07 General Electric Company Thick coated combustor liner

Patent Citations (4)

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Publication number Priority date Publication date Assignee Title
GB2125950A (en) * 1982-08-16 1984-03-14 Gen Electric Gas turbine combustor
US4567730A (en) * 1983-10-03 1986-02-04 General Electric Company Shielded combustor
US5353587A (en) * 1992-06-12 1994-10-11 General Electric Company Film cooling starter geometry for combustor lines
EP1096205A1 (en) * 1999-11-01 2001-05-02 General Electric Company Offset dilution combustion liner

Also Published As

Publication number Publication date
US20050081527A1 (en) 2005-04-21
JP4569952B2 (ja) 2010-10-27
JP2005121352A (ja) 2005-05-12
CN1609427A (zh) 2005-04-27
US7051532B2 (en) 2006-05-30
EP1524472A2 (en) 2005-04-20
BRPI0403055A (pt) 2005-06-28
EP1524472A3 (en) 2012-05-09

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Granted publication date: 20111228

Termination date: 20130817