JP2003227305A5 - - Google Patents

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Publication number
JP2003227305A5
JP2003227305A5 JP2002379699A JP2002379699A JP2003227305A5 JP 2003227305 A5 JP2003227305 A5 JP 2003227305A5 JP 2002379699 A JP2002379699 A JP 2002379699A JP 2002379699 A JP2002379699 A JP 2002379699A JP 2003227305 A5 JP2003227305 A5 JP 2003227305A5
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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.)
Granted
Application number
JP2002379699A
Other versions
JP4130580B2 (ja
JP2003227305A (ja
Filing date
Publication date
Priority claimed from US10/029,227 external-priority patent/US6599089B2/en
Application filed filed Critical
Publication of JP2003227305A publication Critical patent/JP2003227305A/ja
Publication of JP2003227305A5 publication Critical patent/JP2003227305A5/ja
Application granted granted Critical
Publication of JP4130580B2 publication Critical patent/JP4130580B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2002379699A 2001-12-28 2002-12-27 ガスタービンにおける弦ヒンジシールのための補助シール Expired - Fee Related JP4130580B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/029227 2001-12-28
US10/029,227 US6599089B2 (en) 2001-12-28 2001-12-28 Supplemental seal for the chordal hinge seal in a gas turbine

Publications (3)

Publication Number Publication Date
JP2003227305A JP2003227305A (ja) 2003-08-15
JP2003227305A5 true JP2003227305A5 (ja) 2006-02-16
JP4130580B2 JP4130580B2 (ja) 2008-08-06

Family

ID=21847927

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002379699A Expired - Fee Related JP4130580B2 (ja) 2001-12-28 2002-12-27 ガスタービンにおける弦ヒンジシールのための補助シール

Country Status (5)

Country Link
US (1) US6599089B2 (ja)
EP (1) EP1323890B1 (ja)
JP (1) JP4130580B2 (ja)
KR (1) KR100780139B1 (ja)
DE (1) DE60214963T2 (ja)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7094026B2 (en) * 2004-04-29 2006-08-22 General Electric Company System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor
US7052234B2 (en) 2004-06-23 2006-05-30 General Electric Company Turbine vane collar seal
US8070427B2 (en) * 2007-10-31 2011-12-06 General Electric Company Gas turbines having flexible chordal hinge seals
EP2187002A1 (en) 2008-11-12 2010-05-19 Siemens Aktiengesellschaft Gas turbine nozzle arrangement and gas turbine
US8141879B2 (en) * 2009-07-20 2012-03-27 General Electric Company Seals for a turbine engine, and methods of assembling a turbine engine
US8413447B2 (en) * 2009-09-16 2013-04-09 General Electric Company Fuel nozzle cup seal
US9482107B2 (en) 2009-09-28 2016-11-01 Siemens Aktiengesellschaft Gas turbine nozzle arrangement and gas turbine
US20120119449A1 (en) * 2010-11-11 2012-05-17 General Electric Company Transition Piece Sealing Assembly With Seal Overlay
US8613451B2 (en) 2010-11-29 2013-12-24 General Electric Company Cloth seal for turbo-machinery
US9115585B2 (en) * 2011-06-06 2015-08-25 General Electric Company Seal assembly for gas turbine
EP2803824A1 (en) * 2013-05-16 2014-11-19 Siemens Aktiengesellschaft A seal for a turbomachine and a method for construction thereof
CN106605041B (zh) * 2014-09-05 2018-09-11 西门子公司 过渡件-到-涡轮机密封组件
US9828868B2 (en) * 2014-09-11 2017-11-28 United Technologies Corporation Hinged seal using wire mesh
US10443419B2 (en) * 2015-04-30 2019-10-15 Rolls-Royce North American Technologies Inc. Seal for a gas turbine engine assembly
US9863259B2 (en) 2015-05-11 2018-01-09 United Technologies Corporation Chordal seal
US20170051983A1 (en) * 2015-08-18 2017-02-23 Arvos Inc. Flexible seal for a rotary regenerative preheater
US10329937B2 (en) 2016-09-16 2019-06-25 United Technologies Corporation Flowpath component for a gas turbine engine including a chordal seal
US10519807B2 (en) 2017-04-19 2019-12-31 Rolls-Royce Corporation Seal segment retention ring with chordal seal feature
US10968777B2 (en) * 2019-04-24 2021-04-06 Raytheon Technologies Corporation Chordal seal
US11878807B2 (en) * 2020-05-07 2024-01-23 Raytheon Company Adaptive air flow inhibitor seal for aircraft propulsion systems

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4184689A (en) * 1978-10-02 1980-01-22 United Technologies Corporation Seal structure for an axial flow rotary machine
US4645217A (en) 1985-11-29 1987-02-24 United Technologies Corporation Finger seal assembly
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
US4863343A (en) 1988-05-16 1989-09-05 Westinghouse Electric Corp. Turbine vane shroud sealing system
US5149250A (en) * 1991-02-28 1992-09-22 General Electric Company Gas turbine vane assembly seal and support system
US5474306A (en) 1992-11-19 1995-12-12 General Electric Co. Woven seal and hybrid cloth-brush seals for turbine applications
US5372476A (en) * 1993-06-18 1994-12-13 General Electric Company Turbine nozzle support assembly
US5657998A (en) 1994-09-19 1997-08-19 General Electric Company Gas-path leakage seal for a gas turbine
US5509669A (en) 1995-06-19 1996-04-23 General Electric Company Gas-path leakage seal for a gas turbine
US5586773A (en) 1995-06-19 1996-12-24 General Electric Company Gas-path leakage seal for a gas turbine made from metallic mesh
US5934687A (en) 1997-07-07 1999-08-10 General Electric Company Gas-path leakage seal for a turbine
US5915697A (en) * 1997-09-22 1999-06-29 General Electric Company Flexible cloth seal assembly
US6162014A (en) 1998-09-22 2000-12-19 General Electric Company Turbine spline seal and turbine assembly containing such spline seal
US6164656A (en) * 1999-01-29 2000-12-26 General Electric Company Turbine nozzle interface seal and methods

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