JP2016531238A5 - - Google Patents

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Publication number
JP2016531238A5
JP2016531238A5 JP2016540886A JP2016540886A JP2016531238A5 JP 2016531238 A5 JP2016531238 A5 JP 2016531238A5 JP 2016540886 A JP2016540886 A JP 2016540886A JP 2016540886 A JP2016540886 A JP 2016540886A JP 2016531238 A5 JP2016531238 A5 JP 2016531238A5
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JP
Japan
Prior art keywords
blocking device
tip
turbomachine
axial
axially extending
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
JP2016540886A
Other languages
English (en)
Japanese (ja)
Other versions
JP6755798B2 (ja
JP2016531238A (ja
Filing date
Publication date
Priority claimed from US14/017,690 external-priority patent/US9638051B2/en
Application filed filed Critical
Publication of JP2016531238A publication Critical patent/JP2016531238A/ja
Publication of JP2016531238A5 publication Critical patent/JP2016531238A5/ja
Application granted granted Critical
Publication of JP6755798B2 publication Critical patent/JP6755798B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2016540886A 2013-09-04 2014-08-04 異なるサイズ設定の阻止装置のためのエンジェルウイングシールを有するターボ機械バケットおよび関連方法 Active JP6755798B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US14/017,690 2013-09-04
US14/017,690 US9638051B2 (en) 2013-09-04 2013-09-04 Turbomachine bucket having angel wing for differently sized discouragers and related methods
PCT/US2014/049549 WO2015034611A1 (en) 2013-09-04 2014-08-04 Turbomachine bucket having angel wing seal for differently sized discouragers and related methods

Publications (3)

Publication Number Publication Date
JP2016531238A JP2016531238A (ja) 2016-10-06
JP2016531238A5 true JP2016531238A5 (https=) 2017-09-07
JP6755798B2 JP6755798B2 (ja) 2020-09-16

Family

ID=51429364

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2016540886A Active JP6755798B2 (ja) 2013-09-04 2014-08-04 異なるサイズ設定の阻止装置のためのエンジェルウイングシールを有するターボ機械バケットおよび関連方法

Country Status (5)

Country Link
US (1) US9638051B2 (https=)
EP (1) EP3042043B1 (https=)
JP (1) JP6755798B2 (https=)
CN (1) CN105683510B (https=)
WO (1) WO2015034611A1 (https=)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9181815B2 (en) * 2012-05-02 2015-11-10 United Technologies Corporation Shaped rim cavity wing surface
US10683765B2 (en) * 2017-02-14 2020-06-16 General Electric Company Turbine blades having shank features and methods of fabricating the same
US11707819B2 (en) 2018-10-15 2023-07-25 General Electric Company Selectively flexible extension tool
US12194620B2 (en) 2018-10-15 2025-01-14 Oliver Crisipin Robotics Limited Selectively flexible extension tool
US11702955B2 (en) 2019-01-14 2023-07-18 General Electric Company Component repair system and method
US12405187B2 (en) 2019-10-04 2025-09-02 General Electric Company Insertion apparatus for use with rotary machines
US11752622B2 (en) 2020-01-23 2023-09-12 General Electric Company Extension tool having a plurality of links
US11692650B2 (en) 2020-01-23 2023-07-04 General Electric Company Selectively flexible extension tool
US11371437B2 (en) 2020-03-10 2022-06-28 Oliver Crispin Robotics Limited Insertion tool
US12091981B2 (en) 2020-06-11 2024-09-17 General Electric Company Insertion tool and method
US12504616B2 (en) 2021-01-08 2025-12-23 General Electric Company Insertion tool
US12416800B2 (en) 2021-01-08 2025-09-16 General Electric Company Insertion tool
US11459903B1 (en) 2021-06-10 2022-10-04 Solar Turbines Incorporated Redirecting stator flow discourager
US20230194234A1 (en) * 2021-12-16 2023-06-22 Oliver Crispin Robotics Limited System and method of adjusting a tool

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4611744A (en) 1982-06-23 1986-09-16 Refurbished Turbine Components Ltd. Turbine blade repair
US5536143A (en) 1995-03-31 1996-07-16 General Electric Co. Closed circuit steam cooled bucket
US6049978A (en) 1996-12-23 2000-04-18 Recast Airfoil Group Methods for repairing and reclassifying gas turbine engine airfoil parts
JP2001073706A (ja) 1999-09-06 2001-03-21 Ishikawajima Harima Heavy Ind Co Ltd タービン動翼の補修方法
US6390774B1 (en) 2000-02-02 2002-05-21 General Electric Company Gas turbine bucket cooling circuit and related process
CA2334071C (en) 2000-02-23 2005-05-24 Mitsubishi Heavy Industries, Ltd. Gas turbine moving blade
JP2002371802A (ja) 2001-06-14 2002-12-26 Mitsubishi Heavy Ind Ltd ガスタービンにおけるシュラウド一体型動翼と分割環
US6532656B1 (en) 2001-10-10 2003-03-18 General Electric Company Gas turbine engine compressor blade restoration method
US6506016B1 (en) 2001-11-15 2003-01-14 General Electric Company Angel wing seals for blades of a gas turbine and methods for determining angel wing seal profiles
US7234918B2 (en) 2004-12-16 2007-06-26 Siemens Power Generation, Inc. Gap control system for turbine engines
US7335427B2 (en) 2004-12-17 2008-02-26 General Electric Company Preform and method of repairing nickel-base superalloys and components repaired thereby
US7836591B2 (en) 2005-03-17 2010-11-23 Siemens Energy, Inc. Method for forming turbine seal by cold spray process
US7465152B2 (en) 2005-09-16 2008-12-16 General Electric Company Angel wing seals for turbine blades and methods for selecting stator, rotor and wing seal profiles
US7500824B2 (en) 2006-08-22 2009-03-10 General Electric Company Angel wing abradable seal and sealing method
US8277172B2 (en) 2009-03-23 2012-10-02 General Electric Company Apparatus for turbine engine cooling air management
US8282346B2 (en) 2009-04-06 2012-10-09 General Electric Company Methods, systems and/or apparatus relating to seals for turbine engines
US8317465B2 (en) 2009-07-02 2012-11-27 General Electric Company Systems and apparatus relating to turbine engines and seals for turbine engines
EP2366488A1 (de) 2010-03-19 2011-09-21 Siemens Aktiengesellschaft Verfahren zum Wiederaufarbeiten einer Turbinenschaufel mit wenigstens einer Plattform
JP5484990B2 (ja) 2010-03-30 2014-05-07 三菱重工業株式会社 タービン
US8777568B2 (en) 2010-09-30 2014-07-15 General Electric Company Apparatus and methods for cooling platform regions of turbine rotor blades
US20120251291A1 (en) 2011-03-31 2012-10-04 General Electric Company Stator-rotor assemblies with features for enhanced containment of gas flow, and related processes
US8967957B2 (en) 2011-11-03 2015-03-03 General Electric Company Rotating airfoil component of a turbomachine

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