JP4694387B2 - 一体形缶型燃焼器 - Google Patents

一体形缶型燃焼器 Download PDF

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Publication number
JP4694387B2
JP4694387B2 JP2006052424A JP2006052424A JP4694387B2 JP 4694387 B2 JP4694387 B2 JP 4694387B2 JP 2006052424 A JP2006052424 A JP 2006052424A JP 2006052424 A JP2006052424 A JP 2006052424A JP 4694387 B2 JP4694387 B2 JP 4694387B2
Authority
JP
Japan
Prior art keywords
combustor
transition piece
sleeve
flow
head end
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
JP2006052424A
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English (en)
Japanese (ja)
Other versions
JP2006242559A (ja
JP2006242559A5 (enExample
Inventor
スタンリー・ケヴィン・ワイデナー
ケヴィン・ウェストン・マクマハン
トーマス・エドワード・ジョンソン
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
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 JP2006242559A publication Critical patent/JP2006242559A/ja
Publication of JP2006242559A5 publication Critical patent/JP2006242559A5/ja
Application granted granted Critical
Publication of JP4694387B2 publication Critical patent/JP4694387B2/ja
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

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)
JP2006052424A 2005-03-02 2006-02-28 一体形缶型燃焼器 Expired - Fee Related JP4694387B2 (ja)

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
US10/906,688 2005-03-02

Publications (3)

Publication Number Publication Date
JP2006242559A JP2006242559A (ja) 2006-09-14
JP2006242559A5 JP2006242559A5 (enExample) 2009-04-09
JP4694387B2 true JP4694387B2 (ja) 2011-06-08

Family

ID=36293366

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2006052424A Expired - Fee Related JP4694387B2 (ja) 2005-03-02 2006-02-28 一体形缶型燃焼器

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
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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
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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
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US7926283B2 (en) * 2009-02-26 2011-04-19 General Electric Company Gas turbine combustion system cooling arrangement
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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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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
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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
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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
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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
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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
CN1828140B (zh) 2011-11-23
US7082766B1 (en) 2006-08-01

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