CN103185353B - 用于涡轮发动机中的燃烧器组件及其组装方法 - Google Patents

用于涡轮发动机中的燃烧器组件及其组装方法 Download PDF

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Publication number
CN103185353B
CN103185353B CN201210431811.8A CN201210431811A CN103185353B CN 103185353 B CN103185353 B CN 103185353B CN 201210431811 A CN201210431811 A CN 201210431811A CN 103185353 B CN103185353 B CN 103185353B
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CN
China
Prior art keywords
fuel
cooling fluid
chamber
fuel nozzle
cooling
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Application number
CN201210431811.8A
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English (en)
Chinese (zh)
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CN103185353A (zh
Inventor
严钟昊
T.E.约翰逊
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General Electric Company PLC
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General Electric Co
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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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2209/00—Safety arrangements
    • F23D2209/10—Flame flashback
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2209/00—Safety arrangements
    • F23D2209/20—Flame lift-off / stability
    • 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
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
    • 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
    • F23R2900/00018—Manufacturing combustion chamber liners or subparts

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)
  • Fuel-Injection Apparatus (AREA)
CN201210431811.8A 2012-01-03 2012-11-02 用于涡轮发动机中的燃烧器组件及其组装方法 Active CN103185353B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/342,303 US8438851B1 (en) 2012-01-03 2012-01-03 Combustor assembly for use in a turbine engine and methods of assembling same
US13/342303 2012-01-03

Publications (2)

Publication Number Publication Date
CN103185353A CN103185353A (zh) 2013-07-03
CN103185353B true CN103185353B (zh) 2016-12-21

Family

ID=47172450

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210431811.8A Active CN103185353B (zh) 2012-01-03 2012-11-02 用于涡轮发动机中的燃烧器组件及其组装方法

Country Status (5)

Country Link
US (1) US8438851B1 (enExample)
EP (1) EP2613083B1 (enExample)
JP (1) JP6030919B2 (enExample)
CN (1) CN103185353B (enExample)
RU (1) RU2605164C2 (enExample)

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US20170227225A1 (en) * 2016-02-09 2017-08-10 General Electric Company Fuel injectors and methods of fabricating same
US10670271B2 (en) * 2016-09-30 2020-06-02 DOOSAN Heavy Industries Construction Co., LTD Acoustic dampening liner cap and gas turbine combustor including the same
US10788215B2 (en) * 2016-12-21 2020-09-29 General Electric Company Fuel nozzle assembly with flange orifice
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US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
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KR102490477B1 (ko) * 2021-02-03 2023-01-19 두산에너빌리티 주식회사 분사노즐, 연소기 및 이를 포함하는 가스터빈
KR102460001B1 (ko) * 2021-02-17 2022-10-26 두산에너빌리티 주식회사 마이크로 믹서모듈 및 이를 포함하는 연소기
DE102022103746A1 (de) 2022-02-17 2023-08-17 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennersystem zur Erzeugung von Heißgas
US12215866B2 (en) 2022-02-18 2025-02-04 General Electric Company Combustor for a turbine engine having a fuel-air mixer including a set of mixing passages
CN115031259B (zh) * 2022-03-18 2023-06-02 北京航空航天大学 一种燃气轮机燃烧室及其设计方法
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CN102251857A (zh) * 2010-05-20 2011-11-23 通用电气公司 用于冷却涡轮机燃烧器过渡件的系统

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Also Published As

Publication number Publication date
EP2613083B1 (en) 2020-08-12
JP6030919B2 (ja) 2016-11-24
CN103185353A (zh) 2013-07-03
EP2613083A3 (en) 2017-12-20
RU2605164C2 (ru) 2016-12-20
EP2613083A2 (en) 2013-07-10
US8438851B1 (en) 2013-05-14
JP2013139993A (ja) 2013-07-18
RU2012146617A (ru) 2014-05-10

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Effective date of registration: 20240109

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Patentee after: GENERAL ELECTRIC CO. LTD.

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Patentee before: General Electric Co.

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