JP2013256941A5 - - Google Patents

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Publication number
JP2013256941A5
JP2013256941A5 JP2013117429A JP2013117429A JP2013256941A5 JP 2013256941 A5 JP2013256941 A5 JP 2013256941A5 JP 2013117429 A JP2013117429 A JP 2013117429A JP 2013117429 A JP2013117429 A JP 2013117429A JP 2013256941 A5 JP2013256941 A5 JP 2013256941A5
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JP
Japan
Prior art keywords
rotation
nozzle
sealing plate
retaining ring
proximate
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
JP2013117429A
Other languages
English (en)
Japanese (ja)
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JP2013256941A (ja
JP6176709B2 (ja
Filing date
Publication date
Priority claimed from US13/492,180 external-priority patent/US9127557B2/en
Application filed filed Critical
Publication of JP2013256941A publication Critical patent/JP2013256941A/ja
Publication of JP2013256941A5 publication Critical patent/JP2013256941A5/ja
Application granted granted Critical
Publication of JP6176709B2 publication Critical patent/JP6176709B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013117429A 2012-06-08 2013-06-04 ガスタービンシステムのためのノズル取付および封止アセンブリ、ならびに、取付および封止方法 Active JP6176709B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/492,180 US9127557B2 (en) 2012-06-08 2012-06-08 Nozzle mounting and sealing assembly for a gas turbine system and method of mounting and sealing
US13/492,180 2012-06-08

Publications (3)

Publication Number Publication Date
JP2013256941A JP2013256941A (ja) 2013-12-26
JP2013256941A5 true JP2013256941A5 (enExample) 2016-07-21
JP6176709B2 JP6176709B2 (ja) 2017-08-09

Family

ID=48578850

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013117429A Active JP6176709B2 (ja) 2012-06-08 2013-06-04 ガスタービンシステムのためのノズル取付および封止アセンブリ、ならびに、取付および封止方法

Country Status (5)

Country Link
US (1) US9127557B2 (enExample)
EP (1) EP2672070B1 (enExample)
JP (1) JP6176709B2 (enExample)
CN (1) CN103485951B (enExample)
RU (1) RU2645098C2 (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2984318B1 (en) * 2013-04-12 2017-12-27 United Technologies Corporation Gas turbine engine seal
JP5717904B1 (ja) * 2014-08-04 2015-05-13 三菱日立パワーシステムズ株式会社 静翼、ガスタービン、分割環、静翼の改造方法、および、分割環の改造方法
US9696037B2 (en) 2014-10-16 2017-07-04 General Electric Company Liner retaining feature for a combustor
US9689813B2 (en) * 2015-02-27 2017-06-27 The Boeing Company Detecting gaps between fasteners and openings
US10215043B2 (en) 2016-02-24 2019-02-26 United Technologies Corporation Method and device for piston seal anti-rotation
US10502093B2 (en) * 2017-12-13 2019-12-10 Pratt & Whitney Canada Corp. Turbine shroud cooling
US11365640B2 (en) 2019-09-19 2022-06-21 Raytheon Technologies Corporation Seal assembly with anti-rotation lock
US11041397B1 (en) * 2019-12-13 2021-06-22 Raytheon Technologies Corporation Non-metallic side plate seal assembly for a gas turbine engine
CN111846251B (zh) * 2020-07-10 2024-03-19 山东太古飞机工程有限公司 一种用于发动机进气口、排气及尾喷嘴的防沙保护装置

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3062499A (en) * 1960-05-18 1962-11-06 United Aircraft Corp Vane mounting and seal
US4815933A (en) 1987-11-13 1989-03-28 The United States Of America As Represented By The Secretary Of The Air Force Nozzle flange attachment and sealing arrangement
US4883405A (en) 1987-11-13 1989-11-28 The United States Of America As Represented By The Secretary Of The Air Force Turbine nozzle mounting arrangement
US5176496A (en) 1991-09-27 1993-01-05 General Electric Company Mounting arrangements for turbine nozzles
US5618161A (en) * 1995-10-17 1997-04-08 Westinghouse Electric Corporation Apparatus for restraining motion of a turbo-machine stationary vane
US5957657A (en) * 1996-02-26 1999-09-28 Mitisubishi Heavy Industries, Ltd. Method of forming a cooling air passage in a gas turbine stationary blade shroud
US6164903A (en) * 1998-12-22 2000-12-26 United Technologies Corporation Turbine vane mounting arrangement
RU2272151C2 (ru) * 2000-12-28 2006-03-20 Альстом Текнолоджи Лтд Лопатка статора осевой турбины
GB0321056D0 (en) * 2003-09-09 2003-10-08 Rolls Royce Plc Joint arrangement
US7094025B2 (en) * 2003-11-20 2006-08-22 General Electric Company Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction
US7040857B2 (en) * 2004-04-14 2006-05-09 General Electric Company Flexible seal assembly between gas turbine components and methods of installation
JP3892859B2 (ja) * 2004-05-31 2007-03-14 川崎重工業株式会社 タービンノズルの支持構造
US8038389B2 (en) * 2006-01-04 2011-10-18 General Electric Company Method and apparatus for assembling turbine nozzle assembly
US7771164B2 (en) * 2006-12-18 2010-08-10 General Electric Company Method and system for assembling a turbine engine
US7850425B2 (en) * 2007-08-10 2010-12-14 General Electric Company Outer sidewall retention scheme for a singlet first stage nozzle
US8070431B2 (en) * 2007-10-31 2011-12-06 General Electric Company Fully contained retention pin for a turbine nozzle
US20090169361A1 (en) * 2007-12-29 2009-07-02 Michael Scott Cole Cooled turbine nozzle segment
US8171690B2 (en) * 2008-05-28 2012-05-08 3Form, Inc. Countersunk fastener assemblies, panel mounting systems, and methods

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