JP2003329245A5 - - Google Patents

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Publication number
JP2003329245A5
JP2003329245A5 JP2003104717A JP2003104717A JP2003329245A5 JP 2003329245 A5 JP2003329245 A5 JP 2003329245A5 JP 2003104717 A JP2003104717 A JP 2003104717A JP 2003104717 A JP2003104717 A JP 2003104717A JP 2003329245 A5 JP2003329245 A5 JP 2003329245A5
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JP
Japan
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.)
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Application number
JP2003104717A
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JP2003329245A (ja
JP4256709B2 (ja
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Publication date
Priority claimed from US10/119,649 external-priority patent/US6655147B2/en
Application filed filed Critical
Publication of JP2003329245A publication Critical patent/JP2003329245A/ja
Publication of JP2003329245A5 publication Critical patent/JP2003329245A5/ja
Application granted granted Critical
Publication of JP4256709B2 publication Critical patent/JP4256709B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2003104717A 2002-04-10 2003-04-09 ガスタービンエンジンの燃焼器用の環状一体形の波形ライナ Expired - Fee Related JP4256709B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/119,649 2002-04-10
US10/119,649 US6655147B2 (en) 2002-04-10 2002-04-10 Annular one-piece corrugated liner for combustor of a gas turbine engine

Publications (3)

Publication Number Publication Date
JP2003329245A JP2003329245A (ja) 2003-11-19
JP2003329245A5 true JP2003329245A5 (ja) 2006-05-25
JP4256709B2 JP4256709B2 (ja) 2009-04-22

Family

ID=28453992

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003104717A Expired - Fee Related JP4256709B2 (ja) 2002-04-10 2003-04-09 ガスタービンエンジンの燃焼器用の環状一体形の波形ライナ

Country Status (5)

Country Link
US (1) US6655147B2 (ja)
EP (1) EP1353127B1 (ja)
JP (1) JP4256709B2 (ja)
CN (1) CN100529543C (ja)
DE (1) DE60334172D1 (ja)

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US8015818B2 (en) * 2005-02-22 2011-09-13 Siemens Energy, Inc. Cooled transition duct for a gas turbine engine
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DE102005060704A1 (de) * 2005-12-19 2007-06-28 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer
US7908867B2 (en) * 2007-09-14 2011-03-22 Siemens Energy, Inc. Wavy CMC wall hybrid ceramic apparatus
US8202588B2 (en) * 2008-04-08 2012-06-19 Siemens Energy, Inc. Hybrid ceramic structure with internal cooling arrangements
US8327648B2 (en) * 2008-12-09 2012-12-11 Pratt & Whitney Canada Corp. Combustor liner with integrated anti-rotation and removal feature
US8904799B2 (en) * 2009-05-25 2014-12-09 Majed Toqan Tangential combustor with vaneless turbine for use on gas turbine engines
US8327644B2 (en) * 2009-11-06 2012-12-11 Jhrg Inc. Micro-turbine combustor
US8707708B2 (en) * 2010-02-22 2014-04-29 United Technologies Corporation 3D non-axisymmetric combustor liner
RU2530685C2 (ru) * 2010-03-25 2014-10-10 Дженерал Электрик Компани Структуры ударного воздействия для систем охлаждения
US20120208141A1 (en) * 2011-02-14 2012-08-16 General Electric Company Combustor
JP6134732B2 (ja) * 2011-12-05 2017-05-24 ゼネラル・エレクトリック・カンパニイ マルチゾーン燃焼器
US8960525B2 (en) * 2013-01-31 2015-02-24 General Electric Company Brazing process and plate assembly
WO2014123850A1 (en) 2013-02-06 2014-08-14 United Technologies Corporation Gas turbine engine component with upstream-directed cooling film holes
US10174949B2 (en) 2013-02-08 2019-01-08 United Technologies Corporation Gas turbine engine combustor liner assembly with convergent hyperbolic profile
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CN104896514A (zh) * 2015-05-13 2015-09-09 广东电网有限责任公司电力科学研究院 燃气轮机主燃烧室防振隔热壁
CN105605605A (zh) * 2016-01-25 2016-05-25 西北工业大学 一种地面燃机燃烧室的防振冷却壁
US10495309B2 (en) * 2016-02-12 2019-12-03 General Electric Company Surface contouring of a flowpath wall of a gas turbine engine
US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a 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
US10641175B2 (en) 2016-03-25 2020-05-05 General Electric Company Panel fuel injector
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for 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
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
US10738646B2 (en) 2017-06-12 2020-08-11 Raytheon Technologies Corporation Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section
US10612555B2 (en) 2017-06-16 2020-04-07 United Technologies Corporation Geared turbofan with overspeed protection
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel 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
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11898755B2 (en) 2022-06-08 2024-02-13 General Electric Company Combustor with a variable volume primary zone combustion chamber
US11835236B1 (en) 2022-07-05 2023-12-05 General Electric Company Combustor with reverse dilution air introduction
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

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US4696431A (en) * 1985-11-29 1987-09-29 United Technologies Corporation Augmentor liner support band having finger positioners
US4930729A (en) * 1986-05-22 1990-06-05 Rolls-Royce Plc Control of fluid flow
US5181379A (en) 1990-11-15 1993-01-26 General Electric Company Gas turbine engine multi-hole film cooled combustor liner and method of manufacture
US5233828A (en) 1990-11-15 1993-08-10 General Electric Company Combustor liner with circumferentially angled film cooling holes
CA2056592A1 (en) 1990-12-21 1992-06-22 Phillip D. Napoli Multi-hole film cooled combustor liner with slotted film starter
GB9127505D0 (en) 1991-03-11 2013-12-25 Gen Electric Multi-hole film cooled afterburner combustor liner
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US5363654A (en) 1993-05-10 1994-11-15 General Electric Company Recuperative impingement cooling of jet engine components
US5460002A (en) 1993-05-21 1995-10-24 General Electric Company Catalytically-and aerodynamically-assisted liner for gas turbine combustors
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