CN1828140B - 整体式筒形燃烧室 - Google Patents

整体式筒形燃烧室 Download PDF

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Publication number
CN1828140B
CN1828140B CN2006100594081A CN200610059408A CN1828140B CN 1828140 B CN1828140 B CN 1828140B CN 2006100594081 A CN2006100594081 A CN 2006100594081A CN 200610059408 A CN200610059408 A CN 200610059408A CN 1828140 B CN1828140 B CN 1828140B
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CN
China
Prior art keywords
combustion chamber
transition piece
sleeve
piece
cannular
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
CN2006100594081A
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English (en)
Chinese (zh)
Other versions
CN1828140A (zh
Inventor
S·K·威德纳
K·W·麦马翰
T·E·约翰逊
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General Electric Co
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General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of CN1828140A publication Critical patent/CN1828140A/zh
Application granted granted Critical
Publication of CN1828140B publication Critical patent/CN1828140B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/22—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants movable, e.g. to an inoperative position; adjustable, e.g. self-adjusting
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular casing
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings

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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)
CN2006100594081A 2005-03-02 2006-03-02 整体式筒形燃烧室 Expired - Fee Related CN1828140B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/906,688 US7082766B1 (en) 2005-03-02 2005-03-02 One-piece can combustor
US10/906688 2005-03-02

Publications (2)

Publication Number Publication Date
CN1828140A CN1828140A (zh) 2006-09-06
CN1828140B true CN1828140B (zh) 2011-11-23

Family

ID=36293366

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2006100594081A Expired - Fee Related CN1828140B (zh) 2005-03-02 2006-03-02 整体式筒形燃烧室

Country Status (6)

Country Link
US (1) US7082766B1 (enExample)
EP (1) EP1705427B1 (enExample)
JP (1) JP4694387B2 (enExample)
KR (1) KR101240072B1 (enExample)
CN (1) CN1828140B (enExample)
DE (1) DE602006007507D1 (enExample)

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JP5010521B2 (ja) * 2008-03-28 2012-08-29 三菱重工業株式会社 燃焼器尾筒案内治具及びガスタービンの燃焼器の取り外し方法、並びに製造方法
US9038396B2 (en) * 2008-04-08 2015-05-26 General Electric Company Cooling apparatus for combustor transition piece
US20090249791A1 (en) * 2008-04-08 2009-10-08 General Electric Company Transition piece impingement sleeve and method of assembly
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
US8087228B2 (en) * 2008-09-11 2012-01-03 General Electric Company Segmented combustor cap
JP2010085052A (ja) * 2008-10-01 2010-04-15 Mitsubishi Heavy Ind Ltd 燃焼器尾筒およびその設計方法ならびにガスタービン
JP5173720B2 (ja) * 2008-10-01 2013-04-03 三菱重工業株式会社 燃焼器接続構造およびガスタービン
US9822649B2 (en) * 2008-11-12 2017-11-21 General Electric Company Integrated combustor and stage 1 nozzle in a gas turbine and method
US20100170258A1 (en) * 2009-01-06 2010-07-08 General Electric Company Cooling apparatus for combustor transition piece
US20100170257A1 (en) * 2009-01-08 2010-07-08 General Electric Company Cooling a one-piece can combustor and related method
US20100205972A1 (en) * 2009-02-17 2010-08-19 General Electric Company One-piece can combustor with heat transfer surface enhacements
US7926283B2 (en) * 2009-02-26 2011-04-19 General Electric Company Gas turbine combustion system cooling arrangement
US8438856B2 (en) * 2009-03-02 2013-05-14 General Electric Company Effusion cooled one-piece can combustor
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US8516822B2 (en) * 2010-03-02 2013-08-27 General Electric Company Angled vanes in combustor flow sleeve
US8276391B2 (en) * 2010-04-19 2012-10-02 General Electric Company Combustor liner cooling at transition duct interface and related method
US8307655B2 (en) 2010-05-20 2012-11-13 General Electric Company System for cooling turbine combustor transition piece
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US8887508B2 (en) * 2011-03-15 2014-11-18 General Electric Company Impingement sleeve and methods for designing and forming impingement sleeve
US9249679B2 (en) 2011-03-15 2016-02-02 General Electric Company Impingement sleeve and methods for designing and forming impingement sleeve
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US9631812B2 (en) 2013-03-18 2017-04-25 General Electric Company Support frame and method for assembly of a combustion module of a gas turbine
US10436445B2 (en) 2013-03-18 2019-10-08 General Electric Company Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine
US9383104B2 (en) 2013-03-18 2016-07-05 General Electric Company Continuous combustion liner for a combustor of a gas turbine
US9360217B2 (en) 2013-03-18 2016-06-07 General Electric Company Flow sleeve for a combustion module of a gas turbine
US9322556B2 (en) 2013-03-18 2016-04-26 General Electric Company Flow sleeve assembly for a combustion module of a gas turbine combustor
US9316396B2 (en) 2013-03-18 2016-04-19 General Electric Company Hot gas path duct for a combustor of a gas turbine
US9316155B2 (en) 2013-03-18 2016-04-19 General Electric Company System for providing fuel to a combustor
CN104234859B (zh) * 2013-06-07 2016-08-31 常州兰翔机械有限责任公司 一种燃气涡轮起动机用燃油盖的制造方法
US11732892B2 (en) 2013-08-14 2023-08-22 General Electric Company Gas turbomachine diffuser assembly with radial flow splitters
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KR101984396B1 (ko) 2017-09-29 2019-05-30 두산중공업 주식회사 트랜지션 피스, 이를 포함하는 연소기 및 가스 터빈
KR102011903B1 (ko) 2017-10-27 2019-08-19 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
KR102049042B1 (ko) 2017-10-27 2019-11-26 두산중공업 주식회사 연료 노즐 조립체, 이를 포함하는 연소기 및 가스 터빈
KR102046455B1 (ko) 2017-10-30 2019-11-19 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
KR102047368B1 (ko) 2017-10-31 2019-11-21 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
KR20190048905A (ko) 2017-10-31 2019-05-09 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
KR102021129B1 (ko) 2017-10-31 2019-11-04 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
KR102064295B1 (ko) 2017-10-31 2020-01-09 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
KR102019091B1 (ko) 2017-10-31 2019-11-04 두산중공업 주식회사 연료 노즐 조립체, 이를 포함하는 연소기 및 가스 터빈
KR102047369B1 (ko) 2017-11-14 2019-11-21 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
CN108131399B (zh) * 2017-11-20 2019-06-28 北京动力机械研究所 一种发动机轴承座冷却结构
KR102142140B1 (ko) 2018-09-17 2020-08-06 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
US11248797B2 (en) * 2018-11-02 2022-02-15 Chromalloy Gas Turbine Llc Axial stop configuration for a combustion liner
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KR102226740B1 (ko) 2020-01-02 2021-03-11 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
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KR102460672B1 (ko) 2021-01-06 2022-10-27 두산에너빌리티 주식회사 연료 노즐, 연료 노즐 모듈 및 이를 포함하는 연소기
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Also Published As

Publication number Publication date
DE602006007507D1 (de) 2009-08-13
EP1705427B1 (en) 2009-07-01
KR20060096319A (ko) 2006-09-11
JP2006242559A (ja) 2006-09-14
KR101240072B1 (ko) 2013-03-06
CN1828140A (zh) 2006-09-06
EP1705427A1 (en) 2006-09-27
JP4694387B2 (ja) 2011-06-08
US7082766B1 (en) 2006-08-01

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