DE602006007507D1 - Einteilige becherförmige Brennkammer - Google Patents

Einteilige becherförmige Brennkammer

Info

Publication number
DE602006007507D1
DE602006007507D1 DE602006007507T DE602006007507T DE602006007507D1 DE 602006007507 D1 DE602006007507 D1 DE 602006007507D1 DE 602006007507 T DE602006007507 T DE 602006007507T DE 602006007507 T DE602006007507 T DE 602006007507T DE 602006007507 D1 DE602006007507 D1 DE 602006007507D1
Authority
DE
Germany
Prior art keywords
combustion chamber
shaped combustion
piece cup
cup
piece
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 - Lifetime
Application number
DE602006007507T
Other languages
German (de)
English (en)
Inventor
Stanley Kevin Widener
Thomas Edward Johnson
Kevin Weston Mcmahan
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 DE602006007507D1 publication Critical patent/DE602006007507D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F23R3/02—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)
DE602006007507T 2005-03-02 2006-02-27 Einteilige becherförmige Brennkammer Expired - Lifetime DE602006007507D1 (de)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
DE602006007507D1 true DE602006007507D1 (de) 2009-08-13

Family

ID=36293366

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006007507T Expired - Lifetime DE602006007507D1 (de) 2005-03-02 2006-02-27 Einteilige becherförmige Brennkammer

Country Status (6)

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

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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
US20090249791A1 (en) * 2008-04-08 2009-10-08 General Electric Company Transition piece impingement sleeve and method of assembly
US9038396B2 (en) * 2008-04-08 2015-05-26 General Electric Company Cooling apparatus for combustor transition piece
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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US20100257863A1 (en) * 2009-04-13 2010-10-14 General Electric Company Combined convection/effusion cooled one-piece can combustor
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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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US20120186269A1 (en) * 2011-01-25 2012-07-26 General Electric Company Support between transition piece and impingement sleeve in combustor
US9249679B2 (en) 2011-03-15 2016-02-02 General Electric Company Impingement sleeve and methods for designing and forming impingement sleeve
US8887508B2 (en) 2011-03-15 2014-11-18 General Electric Company Impingement sleeve and methods for designing and forming impingement sleeve
US8997501B2 (en) * 2011-06-02 2015-04-07 General Electric Company System for mounting combustor transition piece to frame of gas turbine engine
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US9360217B2 (en) * 2013-03-18 2016-06-07 General Electric Company Flow sleeve for 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
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
US9316155B2 (en) 2013-03-18 2016-04-19 General Electric Company System for providing fuel to a combustor
US9316396B2 (en) 2013-03-18 2016-04-19 General Electric Company Hot gas path duct for a combustor of a gas turbine
US9400114B2 (en) 2013-03-18 2016-07-26 General Electric Company Combustor support assembly for mounting 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
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
FR3022613B1 (fr) * 2014-06-24 2019-04-19 Safran Helicopter Engines Bossage pour chambre de combustion.
EP3002519B1 (en) 2014-09-30 2020-05-27 Ansaldo Energia Switzerland AG Combustor arrangement with fastening system for combustor parts
CN104595926A (zh) * 2015-01-23 2015-05-06 北京华清燃气轮机与煤气化联合循环工程技术有限公司 热通道部件一体燃烧室
US20160281992A1 (en) * 2015-03-24 2016-09-29 General Electric Company Injection boss for a unibody combustor
US9945295B2 (en) * 2015-06-01 2018-04-17 United Technologies Corporation Composite piston ring seal for axially and circumferentially translating ducts
US10197278B2 (en) 2015-09-02 2019-02-05 General Electric Company Combustor assembly for a turbine engine
US10371383B2 (en) * 2017-01-27 2019-08-06 General Electric Company Unitary flow path structure
KR101984396B1 (ko) 2017-09-29 2019-05-30 두산중공업 주식회사 트랜지션 피스, 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
KR102011903B1 (ko) 2017-10-27 2019-08-19 두산중공업 주식회사 연료 노즐, 이를 포함하는 연소기 및 가스 터빈
KR102046455B1 (ko) 2017-10-30 2019-11-19 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
KR102021129B1 (ko) 2017-10-31 2019-11-04 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
KR102064295B1 (ko) 2017-10-31 2020-01-09 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
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
US11377970B2 (en) 2018-11-02 2022-07-05 Chromalloy Gas Turbine Llc System and method for providing compressed air to a gas turbine combustor
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Also Published As

Publication number Publication date
KR101240072B1 (ko) 2013-03-06
CN1828140B (zh) 2011-11-23
US7082766B1 (en) 2006-08-01
CN1828140A (zh) 2006-09-06
KR20060096319A (ko) 2006-09-11
JP2006242559A (ja) 2006-09-14
EP1705427A1 (en) 2006-09-27
EP1705427B1 (en) 2009-07-01
JP4694387B2 (ja) 2011-06-08

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