JP2014112023A5 - - Google Patents

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Publication number
JP2014112023A5
JP2014112023A5 JP2013220700A JP2013220700A JP2014112023A5 JP 2014112023 A5 JP2014112023 A5 JP 2014112023A5 JP 2013220700 A JP2013220700 A JP 2013220700A JP 2013220700 A JP2013220700 A JP 2013220700A JP 2014112023 A5 JP2014112023 A5 JP 2014112023A5
Authority
JP
Japan
Prior art keywords
wall
socket
combustor
axial
cooling
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.)
Ceased
Application number
JP2013220700A
Other languages
English (en)
Japanese (ja)
Other versions
JP2014112023A (ja
Filing date
Publication date
Priority claimed from US13/665,236 external-priority patent/US9188336B2/en
Application filed filed Critical
Publication of JP2014112023A publication Critical patent/JP2014112023A/ja
Publication of JP2014112023A5 publication Critical patent/JP2014112023A5/ja
Ceased legal-status Critical Current

Links

JP2013220700A 2012-10-31 2013-10-24 タービン・エンジンの燃焼器冷却に関係するアセンブリ及び装置 Ceased JP2014112023A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/665,236 US9188336B2 (en) 2012-10-31 2012-10-31 Assemblies and apparatus related to combustor cooling in turbine engines
US13/665,236 2012-10-31

Publications (2)

Publication Number Publication Date
JP2014112023A JP2014112023A (ja) 2014-06-19
JP2014112023A5 true JP2014112023A5 (enExample) 2016-12-08

Family

ID=49485609

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013220700A Ceased JP2014112023A (ja) 2012-10-31 2013-10-24 タービン・エンジンの燃焼器冷却に関係するアセンブリ及び装置

Country Status (3)

Country Link
US (1) US9188336B2 (enExample)
EP (1) EP2728259A1 (enExample)
JP (1) JP2014112023A (enExample)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3102883B1 (en) * 2014-02-03 2020-04-01 United Technologies Corporation Film cooling a combustor wall of a turbine engine
US20150338101A1 (en) * 2014-05-21 2015-11-26 General Electric Company Turbomachine combustor including a combustor sleeve baffle
US9803864B2 (en) * 2014-06-24 2017-10-31 General Electric Company Turbine air flow conditioner
WO2016013585A1 (ja) * 2014-07-25 2016-01-28 三菱日立パワーシステムズ株式会社 燃焼器用筒体、燃焼器及びガスタービン
US9945294B2 (en) * 2015-12-22 2018-04-17 General Electric Company Staged fuel and air injection in combustion systems of gas turbines
US11098653B2 (en) * 2018-01-12 2021-08-24 Raytheon Technologies Corporation Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
US11371703B2 (en) * 2018-01-12 2022-06-28 Raytheon Technologies Corporation Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
US11988145B2 (en) * 2018-01-12 2024-05-21 Rtx Corporation Apparatus and method for mitigating airflow separation around engine combustor
KR102051988B1 (ko) * 2018-03-28 2019-12-04 두산중공업 주식회사 이중관 라이너 내부 유동가이드를 포함하는 가스 터빈 엔진의 연소기, 및 이를 포함하는 가스터빈
JP7392596B2 (ja) * 2020-07-13 2023-12-06 株式会社デンソー 冷却装置
US11629857B2 (en) * 2021-03-31 2023-04-18 General Electric Company Combustor having a wake energizer

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4719748A (en) 1985-05-14 1988-01-19 General Electric Company Impingement cooled transition duct
US5419115A (en) * 1994-04-29 1995-05-30 United Technologies Corporation Bulkhead and fuel nozzle guide assembly for an annular combustion chamber
US7721548B2 (en) * 2006-11-17 2010-05-25 Pratt & Whitney Canada Corp. Combustor liner and heat shield assembly
US8281600B2 (en) 2007-01-09 2012-10-09 General Electric Company Thimble, sleeve, and method for cooling a combustor assembly
US8166764B2 (en) 2008-07-21 2012-05-01 United Technologies Corporation Flow sleeve impingement cooling using a plenum ring
US20100037622A1 (en) 2008-08-18 2010-02-18 General Electric Company Contoured Impingement Sleeve Holes
US8646276B2 (en) 2009-11-11 2014-02-11 General Electric Company Combustor assembly for a turbine engine with enhanced cooling
US8276391B2 (en) * 2010-04-19 2012-10-02 General Electric Company Combustor liner cooling at transition duct interface and related method
US20120198855A1 (en) * 2011-02-03 2012-08-09 General Electric Company Method and apparatus for cooling combustor liner in combustor

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