JP5802493B2 - 摩耗性バケットシュラウド - Google Patents

摩耗性バケットシュラウド Download PDF

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Publication number
JP5802493B2
JP5802493B2 JP2011197910A JP2011197910A JP5802493B2 JP 5802493 B2 JP5802493 B2 JP 5802493B2 JP 2011197910 A JP2011197910 A JP 2011197910A JP 2011197910 A JP2011197910 A JP 2011197910A JP 5802493 B2 JP5802493 B2 JP 5802493B2
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Japan
Prior art keywords
bucket
shroud
wearable
curved surface
ridges
Prior art date
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Expired - Fee Related
Application number
JP2011197910A
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English (en)
Japanese (ja)
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JP2012062887A5 (https=
JP2012062887A (ja
Inventor
ジェムス・アルバート・トールマン
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2012062887A publication Critical patent/JP2012062887A/ja
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Application granted granted Critical
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Expired - Fee Related legal-status Critical Current
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP2011197910A 2010-09-15 2011-09-12 摩耗性バケットシュラウド Expired - Fee Related JP5802493B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/882,311 US8579581B2 (en) 2010-09-15 2010-09-15 Abradable bucket shroud
US12/882,311 2010-09-15

Publications (3)

Publication Number Publication Date
JP2012062887A JP2012062887A (ja) 2012-03-29
JP2012062887A5 JP2012062887A5 (https=) 2014-10-30
JP5802493B2 true JP5802493B2 (ja) 2015-10-28

Family

ID=45756218

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011197910A Expired - Fee Related JP5802493B2 (ja) 2010-09-15 2011-09-12 摩耗性バケットシュラウド

Country Status (5)

Country Link
US (1) US8579581B2 (https=)
JP (1) JP5802493B2 (https=)
CN (1) CN102434220B (https=)
CH (1) CH703758B1 (https=)
DE (1) DE102011053048B4 (https=)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9598969B2 (en) 2012-07-20 2017-03-21 Kabushiki Kaisha Toshiba Turbine, manufacturing method thereof, and power generating system
JP5951387B2 (ja) * 2012-07-20 2016-07-13 株式会社東芝 ラビリンスシール部およびタービン
CN103883361B (zh) * 2012-12-20 2016-05-04 中航商用航空发动机有限责任公司 涡轮叶片
WO2014171997A2 (en) 2013-02-28 2014-10-23 United Technologies Corporation Contoured blade outer air seal for a gas turbine engine
US9816392B2 (en) * 2013-04-10 2017-11-14 General Electric Company Architectures for high temperature TBCs with ultra low thermal conductivity and abradability and method of making
CN103422912B (zh) * 2013-08-29 2015-04-08 哈尔滨工程大学 一种包括叶顶带有孔窝的动叶片的涡轮
US8939706B1 (en) 2014-02-25 2015-01-27 Siemens Energy, Inc. Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface
US8939707B1 (en) * 2014-02-25 2015-01-27 Siemens Energy, Inc. Turbine abradable layer with progressive wear zone terraced ridges
US9249680B2 (en) 2014-02-25 2016-02-02 Siemens Energy, Inc. Turbine abradable layer with asymmetric ridges or grooves
US9151175B2 (en) 2014-02-25 2015-10-06 Siemens Aktiengesellschaft Turbine abradable layer with progressive wear zone multi level ridge arrays
US8939716B1 (en) 2014-02-25 2015-01-27 Siemens Aktiengesellschaft Turbine abradable layer with nested loop groove pattern
US8939705B1 (en) 2014-02-25 2015-01-27 Siemens Energy, Inc. Turbine abradable layer with progressive wear zone multi depth grooves
US9243511B2 (en) 2014-02-25 2016-01-26 Siemens Aktiengesellschaft Turbine abradable layer with zig zag groove pattern
RU2016134446A (ru) 2014-02-25 2018-03-29 Сименс Акциенгезелльшафт Термобарьерное покрытие компонента турбины с изменяющимися по глубине свойствами материала
JP6290438B2 (ja) * 2014-02-25 2018-03-07 シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft タービンエンジン
KR102318300B1 (ko) 2014-05-15 2021-10-29 누보 피그노네 에스알엘 터보기계의 구성요소의 제조 방법, 터보기계의 구성요소 및 터보기계
US10190435B2 (en) 2015-02-18 2019-01-29 Siemens Aktiengesellschaft Turbine shroud with abradable layer having ridges with holes
EP3259452A2 (en) 2015-02-18 2017-12-27 Siemens Aktiengesellschaft Forming cooling passages in combustion turbine superalloy castings
CN112031878A (zh) * 2020-11-05 2020-12-04 中国航发沈阳黎明航空发动机有限责任公司 一种涡轮转子叶片叶尖双层壁结构

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3019920C2 (de) * 1980-05-24 1982-12-30 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur äußeren Ummantelung der Laufschaufeln von Axialturbinen für Gasturbinentriebwerke
JPH10266804A (ja) * 1997-03-26 1998-10-06 Mitsubishi Heavy Ind Ltd チップシュラウド翼キャビティ
US6660405B2 (en) 2001-05-24 2003-12-09 General Electric Co. High temperature abradable coating for turbine shrouds without bucket tipping
FR2832180B1 (fr) * 2001-11-14 2005-02-18 Snecma Moteurs Revetement abradable pour parois de turbines a gaz
US6887528B2 (en) 2002-12-17 2005-05-03 General Electric Company High temperature abradable coatings
US20050003172A1 (en) * 2002-12-17 2005-01-06 General Electric Company 7FAstage 1 abradable coatings and method for making same
US6916529B2 (en) 2003-01-09 2005-07-12 General Electric Company High temperature, oxidation-resistant abradable coatings containing microballoons and method for applying same
EP1591626A1 (de) * 2004-04-30 2005-11-02 Alstom Technology Ltd Schaufel für Gasturbine
US7614847B2 (en) * 2004-11-24 2009-11-10 General Electric Company Pattern for the surface of a turbine shroud
US7600968B2 (en) 2004-11-24 2009-10-13 General Electric Company Pattern for the surface of a turbine shroud
EP1715140A1 (de) * 2005-04-21 2006-10-25 Siemens Aktiengesellschaft Turbinenschaufel mit einer Deckplatte und einer auf der Deckplatte aufgebrachte Schutzschicht
US7500824B2 (en) 2006-08-22 2009-03-10 General Electric Company Angel wing abradable seal and sealing method
US8622784B2 (en) 2008-07-02 2014-01-07 Huffman Corporation Method for selectively removing portions of an abradable coating using a water jet

Also Published As

Publication number Publication date
CH703758B1 (de) 2016-02-15
US8579581B2 (en) 2013-11-12
CH703758A2 (de) 2012-03-15
US20120063881A1 (en) 2012-03-15
DE102011053048B4 (de) 2022-07-21
JP2012062887A (ja) 2012-03-29
CN102434220A (zh) 2012-05-02
DE102011053048A1 (de) 2012-03-15
CN102434220B (zh) 2015-08-26

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