DE69523545T2 - Verstärkungrahmen für Gasturbinenbrennkammerendstück - Google Patents

Verstärkungrahmen für Gasturbinenbrennkammerendstück

Info

Publication number
DE69523545T2
DE69523545T2 DE69523545T DE69523545T DE69523545T2 DE 69523545 T2 DE69523545 T2 DE 69523545T2 DE 69523545 T DE69523545 T DE 69523545T DE 69523545 T DE69523545 T DE 69523545T DE 69523545 T2 DE69523545 T2 DE 69523545T2
Authority
DE
Germany
Prior art keywords
transition piece
wall
frame
gas turbine
radially inner
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
DE69523545T
Other languages
German (de)
English (en)
Other versions
DE69523545D1 (de
Inventor
Rodger Orval Anderson
John Eugene Barnes
Charles Evan Steber
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 DE69523545D1 publication Critical patent/DE69523545D1/de
Application granted granted Critical
Publication of DE69523545T2 publication Critical patent/DE69523545T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F23R3/42—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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69523545T 1994-12-20 1995-11-30 Verstärkungrahmen für Gasturbinenbrennkammerendstück Expired - Fee Related DE69523545T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US35949594A 1994-12-20 1994-12-20

Publications (2)

Publication Number Publication Date
DE69523545D1 DE69523545D1 (de) 2001-12-06
DE69523545T2 true DE69523545T2 (de) 2002-05-29

Family

ID=23414052

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69523545T Expired - Fee Related DE69523545T2 (de) 1994-12-20 1995-11-30 Verstärkungrahmen für Gasturbinenbrennkammerendstück

Country Status (4)

Country Link
US (1) US5761898A (enExample)
EP (1) EP0718468B1 (enExample)
JP (1) JP3727987B2 (enExample)
DE (1) DE69523545T2 (enExample)

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US7726959B2 (en) * 1998-07-31 2010-06-01 The Texas A&M University Gerotor apparatus for a quasi-isothermal Brayton cycle engine
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US20100003152A1 (en) * 2004-01-23 2010-01-07 The Texas A&M University System Gerotor apparatus for a quasi-isothermal brayton cycle engine
BR0307457A (pt) * 2002-02-05 2005-05-10 Texas A & M Univ Sys Aparelho gerotor para um motor de ciclo de brayton quasi-isotérmico
US6662567B1 (en) 2002-08-14 2003-12-16 Power Systems Mfg, Llc Transition duct mounting system
DE10239534A1 (de) * 2002-08-23 2004-04-22 Man Turbomaschinen Ag Heißgas führendes Gassammelrohr
US6644032B1 (en) * 2002-10-22 2003-11-11 Power Systems Mfg, Llc Transition duct with enhanced profile optimization
US6860108B2 (en) * 2003-01-22 2005-03-01 Mitsubishi Heavy Industries, Ltd. Gas turbine tail tube seal and gas turbine using the same
US7663283B2 (en) * 2003-02-05 2010-02-16 The Texas A & M University System Electric machine having a high-torque switched reluctance motor
KR100908234B1 (ko) * 2003-02-13 2009-07-20 삼성모바일디스플레이주식회사 전계 발광 표시 장치 및 이의 제조방법
BRPI0518276A2 (pt) * 2004-10-22 2008-11-11 Texas A & M Univ Sys aparelho gerotor para um motor de ciclo de brayton quase isotÉrmico
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US8230688B2 (en) * 2008-09-29 2012-07-31 Siemens Energy, Inc. Modular transvane assembly
US8491259B2 (en) * 2009-08-26 2013-07-23 Siemens Energy, Inc. Seal system between transition duct exit section and turbine inlet in a gas turbine engine
US8511972B2 (en) * 2009-12-16 2013-08-20 Siemens Energy, Inc. Seal member for use in a seal system between a transition duct exit section and a turbine inlet in a gas turbine engine
US8978388B2 (en) 2011-06-03 2015-03-17 General Electric Company Load member for transition duct in turbine system
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US8448450B2 (en) 2011-07-05 2013-05-28 General Electric Company Support assembly for transition duct in turbine system
US8650852B2 (en) 2011-07-05 2014-02-18 General Electric Company Support assembly for transition duct in turbine system
JP5848074B2 (ja) * 2011-09-16 2016-01-27 三菱日立パワーシステムズ株式会社 ガスタービン、尾筒及び燃焼器
US8459041B2 (en) 2011-11-09 2013-06-11 General Electric Company Leaf seal for transition duct in turbine system
US8974179B2 (en) 2011-11-09 2015-03-10 General Electric Company Convolution seal for transition duct in turbine system
US8701415B2 (en) 2011-11-09 2014-04-22 General Electric Company Flexible metallic seal for transition duct in turbine system
US20130236301A1 (en) * 2012-03-09 2013-09-12 General Electric Company Apparatus And System For Directing Hot Gas
US20130255276A1 (en) * 2012-03-27 2013-10-03 Alstom Technology Ltd. Transition Duct Mounting System
US9506359B2 (en) 2012-04-03 2016-11-29 General Electric Company Transition nozzle combustion system
US9038394B2 (en) 2012-04-30 2015-05-26 General Electric Company Convolution seal for transition duct in turbine system
US9133722B2 (en) 2012-04-30 2015-09-15 General Electric Company Transition duct with late injection in turbine system
US9249678B2 (en) 2012-06-27 2016-02-02 General Electric Company Transition duct for a gas turbine
US8707673B1 (en) 2013-01-04 2014-04-29 General Electric Company Articulated transition duct in turbomachine
US9322335B2 (en) 2013-03-15 2016-04-26 Siemens Energy, Inc. Gas turbine combustor exit piece with hinged connections
US9080447B2 (en) 2013-03-21 2015-07-14 General Electric Company Transition duct with divided upstream and downstream portions
US9458732B2 (en) 2013-10-25 2016-10-04 General Electric Company Transition duct assembly with modified trailing edge in turbine system
US10072514B2 (en) 2014-07-17 2018-09-11 Siemens Energy, Inc. Method and apparatus for attaching a transition duct to a turbine section in a gas turbine engine
US9359955B2 (en) * 2014-08-28 2016-06-07 Siemens Energy, Inc. Apparatus and method incorporating a transition AFT support for a gas turbine engine
WO2016080957A1 (en) * 2014-11-18 2016-05-26 Siemens Aktiengesellschaft Transition duct exit frame with insert
EP3783200B1 (en) 2014-12-11 2024-03-06 Siemens Energy Global GmbH & Co. KG Transition duct for a gas turbine engine
US10520193B2 (en) 2015-10-28 2019-12-31 General Electric Company Cooling patch for hot gas path components
US10260360B2 (en) * 2016-03-24 2019-04-16 General Electric Company Transition duct assembly
US10260752B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly with late injection features
US10227883B2 (en) 2016-03-24 2019-03-12 General Electric Company Transition duct assembly
US10260424B2 (en) 2016-03-24 2019-04-16 General Electric Company Transition duct assembly with late injection features
US10145251B2 (en) 2016-03-24 2018-12-04 General Electric Company Transition duct assembly
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
US10584876B2 (en) 2016-03-25 2020-03-10 General Electric Company Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
US10655541B2 (en) 2016-03-25 2020-05-19 General Electric Company Segmented annular combustion system
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
US10520194B2 (en) 2016-03-25 2019-12-31 General Electric Company Radially stacked fuel injection module for a segmented annular combustion system
US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
US11022240B2 (en) 2017-06-12 2021-06-01 General Electric Company Cooling and insulating manifold seal assembly for a propulsion system
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
DE112022001110T5 (de) * 2021-02-18 2024-01-18 Siemens Energy Global GmbH & Co. KG Übergang mit unebener Fläche
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

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Also Published As

Publication number Publication date
JPH08261017A (ja) 1996-10-08
US5761898A (en) 1998-06-09
JP3727987B2 (ja) 2005-12-21
DE69523545D1 (de) 2001-12-06
EP0718468B1 (en) 2001-10-31
EP0718468A1 (en) 1996-06-26

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN

8339 Ceased/non-payment of the annual fee