JP6067216B2 - 接合タービンバケット先端シュラウド及び関連する方法 - Google Patents

接合タービンバケット先端シュラウド及び関連する方法 Download PDF

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Publication number
JP6067216B2
JP6067216B2 JP2011225400A JP2011225400A JP6067216B2 JP 6067216 B2 JP6067216 B2 JP 6067216B2 JP 2011225400 A JP2011225400 A JP 2011225400A JP 2011225400 A JP2011225400 A JP 2011225400A JP 6067216 B2 JP6067216 B2 JP 6067216B2
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JP
Japan
Prior art keywords
tip shroud
turbine bucket
airfoil
bucket
metallic material
Prior art date
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JP2011225400A
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English (en)
Japanese (ja)
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JP2012087787A (ja
JP2012087787A5 (enExample
Inventor
ゲーリー・チャールズ・リオッタ
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
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
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Publication of JP2012087787A5 publication Critical patent/JP2012087787A5/ja
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Publication of JP6067216B2 publication Critical patent/JP6067216B2/ja
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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
    • 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
    • F01D5/14Form or construction
    • F01D5/147Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/17Alloys
    • F05D2300/175Superalloys
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/605Crystalline
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/612Foam
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP2011225400A 2010-10-19 2011-10-13 接合タービンバケット先端シュラウド及び関連する方法 Active JP6067216B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/907,432 US8753093B2 (en) 2010-10-19 2010-10-19 Bonded turbine bucket tip shroud and related method
US12/907,432 2010-10-19

Publications (3)

Publication Number Publication Date
JP2012087787A JP2012087787A (ja) 2012-05-10
JP2012087787A5 JP2012087787A5 (enExample) 2014-11-27
JP6067216B2 true JP6067216B2 (ja) 2017-01-25

Family

ID=45895948

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011225400A Active JP6067216B2 (ja) 2010-10-19 2011-10-13 接合タービンバケット先端シュラウド及び関連する方法

Country Status (5)

Country Link
US (1) US8753093B2 (enExample)
JP (1) JP6067216B2 (enExample)
CN (1) CN102454424B (enExample)
DE (1) DE102011054588B4 (enExample)
FR (1) FR2966192B1 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102926819A (zh) * 2012-10-23 2013-02-13 如皋透平叶片制造有限公司 一种汽轮机叶片防窜动叶冠
US20140255194A1 (en) * 2012-12-21 2014-09-11 General Electric Company Tip shrouds of turbine rotor blades and methods of manufacture related thereto
US9321115B2 (en) * 2014-02-05 2016-04-26 Alstom Technologies Ltd Method of repairing a transition duct side seal
GB201403588D0 (en) 2014-02-28 2014-04-16 Rolls Royce Plc Blade tip
US20170053678A1 (en) 2015-08-20 2017-02-23 HGST Netherlands B.V. Adhesive cover seal for hermetically-sealed data storage device
US9852777B2 (en) 2016-02-17 2017-12-26 Western Digital Technologies, Inc. Hermetically-sealed hard disk drive cover perimeter adhesive seal
US9818454B1 (en) 2016-06-22 2017-11-14 Western Digital Technologies, Inc. Hermetically-sealed data storage device for increased disk diameter
FR3071538B1 (fr) * 2017-09-27 2020-09-04 Safran Aircraft Engines Aube de rotor pour une turbomachine

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3527544A (en) 1968-12-12 1970-09-08 Gen Motors Corp Cooled blade shroud
DE2401951A1 (de) * 1973-01-17 1974-07-25 Rolls Royce 1971 Ltd Dichtungsanordnung fuer turbomaschinen
US4285108A (en) * 1979-02-23 1981-08-25 United Technologies Corporation Apparatus and method for refinishing turbine blade airseals
US4390320A (en) * 1980-05-01 1983-06-28 General Electric Company Tip cap for a rotor blade and method of replacement
US4822248A (en) * 1987-04-15 1989-04-18 Metallurgical Industries, Inc. Rebuilt shrouded turbine blade and method of rebuilding the same
US5584663A (en) 1994-08-15 1996-12-17 General Electric Company Environmentally-resistant turbine blade tip
US6164916A (en) * 1998-11-02 2000-12-26 General Electric Company Method of applying wear-resistant materials to turbine blades, and turbine blades having wear-resistant materials
EP1143030A1 (en) 2000-04-03 2001-10-10 ABB Alstom Power N.V. Tip material for a turbine blade and method of manufacturing or repairing a tip of a turbine blade
US6468040B1 (en) 2000-07-24 2002-10-22 General Electric Company Environmentally resistant squealer tips and method for making
EP1186748A1 (de) 2000-09-05 2002-03-13 Siemens Aktiengesellschaft Laufschaufel für eine Strömungsmaschine sowie Strömungsmaschine
JP3801452B2 (ja) * 2001-02-28 2006-07-26 三菱重工業株式会社 耐摩耗性コーティング及びその施工方法
US6506022B2 (en) 2001-04-27 2003-01-14 General Electric Company Turbine blade having a cooled tip shroud
CN1205357C (zh) * 2001-05-31 2005-06-08 三菱重工业株式会社 保护膜形成方法、保护膜形成用材料及研磨性保护膜形成用薄板
US6616410B2 (en) 2001-11-01 2003-09-09 General Electric Company Oxidation resistant and/or abrasion resistant squealer tip and method for casting same
JP2003148103A (ja) * 2001-11-09 2003-05-21 Mitsubishi Heavy Ind Ltd タービンおよびその製造方法
US6869270B2 (en) 2002-06-06 2005-03-22 General Electric Company Turbine blade cover cooling apparatus and method of fabrication
US6926495B2 (en) * 2003-09-12 2005-08-09 Siemens Westinghouse Power Corporation Turbine blade tip clearance control device
US6994920B2 (en) 2003-10-31 2006-02-07 General Electric Company Fusion welding method and welded article
EP1715140A1 (de) * 2005-04-21 2006-10-25 Siemens Aktiengesellschaft Turbinenschaufel mit einer Deckplatte und einer auf der Deckplatte aufgebrachte Schutzschicht
US7771171B2 (en) 2006-12-14 2010-08-10 General Electric Company Systems for preventing wear on turbine blade tip shrouds

Also Published As

Publication number Publication date
CN102454424A (zh) 2012-05-16
JP2012087787A (ja) 2012-05-10
DE102011054588B4 (de) 2025-01-16
FR2966192B1 (fr) 2017-12-08
FR2966192A1 (fr) 2012-04-20
US20120093634A1 (en) 2012-04-19
CN102454424B (zh) 2015-11-25
US8753093B2 (en) 2014-06-17
DE102011054588A1 (de) 2012-04-19

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