JP2015524911A5 - - Google Patents

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Publication number
JP2015524911A5
JP2015524911A5 JP2015525581A JP2015525581A JP2015524911A5 JP 2015524911 A5 JP2015524911 A5 JP 2015524911A5 JP 2015525581 A JP2015525581 A JP 2015525581A JP 2015525581 A JP2015525581 A JP 2015525581A JP 2015524911 A5 JP2015524911 A5 JP 2015524911A5
Authority
JP
Japan
Prior art keywords
inner annular
piston ring
burner tube
annular hub
cap assembly
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.)
Granted
Application number
JP2015525581A
Other languages
English (en)
Japanese (ja)
Other versions
JP2015524911A (ja
JP6212555B2 (ja
Filing date
Publication date
Priority claimed from US13/566,286 external-priority patent/US9003803B2/en
Application filed filed Critical
Publication of JP2015524911A publication Critical patent/JP2015524911A/ja
Publication of JP2015524911A5 publication Critical patent/JP2015524911A5/ja
Application granted granted Critical
Publication of JP6212555B2 publication Critical patent/JP6212555B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2015525581A 2012-08-03 2013-08-01 燃焼器キャップアセンブリ Active JP6212555B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/566,286 US9003803B2 (en) 2012-08-03 2012-08-03 Combustor cap assembly
US13/566,286 2012-08-03
PCT/US2013/053146 WO2014022627A1 (en) 2012-08-03 2013-08-01 Combustor cap assembly

Publications (3)

Publication Number Publication Date
JP2015524911A JP2015524911A (ja) 2015-08-27
JP2015524911A5 true JP2015524911A5 (enExample) 2016-09-08
JP6212555B2 JP6212555B2 (ja) 2017-10-11

Family

ID=48948554

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015525581A Active JP6212555B2 (ja) 2012-08-03 2013-08-01 燃焼器キャップアセンブリ

Country Status (5)

Country Link
US (1) US9003803B2 (enExample)
JP (1) JP6212555B2 (enExample)
CH (1) CH708653B1 (enExample)
DE (1) DE112013003847B4 (enExample)
WO (1) WO2014022627A1 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9423136B2 (en) * 2013-12-13 2016-08-23 General Electric Company Bundled tube fuel injector aft plate retention
CN106325372A (zh) * 2015-06-30 2017-01-11 联想(北京)有限公司 电子设备和模式切换方法
CN106325373B (zh) * 2015-06-30 2024-06-21 联想(北京)有限公司 电子设备和信息处理方法
US10429073B2 (en) * 2015-12-21 2019-10-01 General Electric Company Combustor cap module and retention system therefor
KR102363311B1 (ko) * 2017-10-30 2022-02-14 두산중공업 주식회사 연소기 및 이를 포함하는 가스 터빈
KR20190048053A (ko) 2017-10-30 2019-05-09 두산중공업 주식회사 연소기 및 이를 포함하는 가스 터빈
CN113739203B (zh) * 2021-09-13 2023-03-10 中国联合重型燃气轮机技术有限公司 用于燃烧器的罩帽组件

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69306025T2 (de) 1992-03-30 1997-05-28 Gen Electric Konstruktion eines Brennkammerdomes
US5274991A (en) 1992-03-30 1994-01-04 General Electric Company Dry low NOx multi-nozzle combustion liner cap assembly
US6438959B1 (en) 2000-12-28 2002-08-27 General Electric Company Combustion cap with integral air diffuser and related method
US6910336B2 (en) 2003-02-18 2005-06-28 Power Systems Mfg. Llc Combustion liner cap assembly attachment and sealing system
US20060230763A1 (en) * 2005-04-13 2006-10-19 General Electric Company Combustor and cap assemblies for combustors in a gas turbine
US7647779B2 (en) * 2005-04-27 2010-01-19 United Technologies Corporation Compliant metal support for ceramic combustor liner in a gas turbine engine
US7827797B2 (en) * 2006-09-05 2010-11-09 General Electric Company Injection assembly for a combustor
US8438853B2 (en) 2008-01-29 2013-05-14 Alstom Technology Ltd. Combustor end cap assembly
US8087228B2 (en) 2008-09-11 2012-01-03 General Electric Company Segmented combustor cap
US8490400B2 (en) * 2008-09-15 2013-07-23 Siemens Energy, Inc. Combustor assembly comprising a combustor device, a transition duct and a flow conditioner
US8171737B2 (en) 2009-01-16 2012-05-08 General Electric Company Combustor assembly and cap for a turbine engine
US8528336B2 (en) * 2009-03-30 2013-09-10 General Electric Company Fuel nozzle spring support for shifting a natural frequency

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