JP4874329B2 - カバープレートとこのカバープレートに被着された保護層とを備えたタービン翼 - Google Patents

カバープレートとこのカバープレートに被着された保護層とを備えたタービン翼 Download PDF

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Publication number
JP4874329B2
JP4874329B2 JP2008507029A JP2008507029A JP4874329B2 JP 4874329 B2 JP4874329 B2 JP 4874329B2 JP 2008507029 A JP2008507029 A JP 2008507029A JP 2008507029 A JP2008507029 A JP 2008507029A JP 4874329 B2 JP4874329 B2 JP 4874329B2
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JP
Japan
Prior art keywords
turbine
blade
cover plate
protective layer
shroud
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.)
Expired - Fee Related
Application number
JP2008507029A
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English (en)
Japanese (ja)
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JP2008538399A (ja
JP2008538399A5 (enExample
Inventor
シュライ、アルベルト
シュヴァス、ゲルハルト
ラッツァー、アルミン デ
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Siemens AG
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Siemens AG
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Publication of JP2008538399A5 publication Critical patent/JP2008538399A5/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
    • 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
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/04Heavy metals
    • F05C2201/0433Iron group; Ferrous alloys, e.g. steel
    • F05C2201/0463Cobalt
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2230/00Manufacture
    • F05D2230/30Manufacture with deposition of material
    • 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
    • F05D2230/00Manufacture
    • F05D2230/30Manufacture with deposition of material
    • F05D2230/31Layer deposition
    • F05D2230/312Layer deposition by plasma spraying
    • 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
    • F05D2230/00Manufacture
    • F05D2230/30Manufacture with deposition of material
    • F05D2230/31Layer deposition
    • F05D2230/313Layer deposition by physical vapour deposition
    • 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
    • F05D2230/00Manufacture
    • F05D2230/90Coating; Surface treatment
    • 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
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/22Non-oxide ceramics
    • F05D2300/226Carbides
    • 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
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/22Non-oxide ceramics
    • F05D2300/228Nitrides
    • 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
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/22Non-oxide ceramics
    • F05D2300/228Nitrides
    • F05D2300/2284Nitrides of titanium
    • 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)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
JP2008507029A 2005-04-21 2006-01-20 カバープレートとこのカバープレートに被着された保護層とを備えたタービン翼 Expired - Fee Related JP4874329B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP05008811.1 2005-04-21
EP05008811A EP1715140A1 (de) 2005-04-21 2005-04-21 Turbinenschaufel mit einer Deckplatte und einer auf der Deckplatte aufgebrachte Schutzschicht
PCT/EP2006/050337 WO2006111427A1 (de) 2005-04-21 2006-01-20 Turbinenschaufel mit einer deckplatte und einer auf der deckplatte aufgebrachte schutzschicht

Publications (3)

Publication Number Publication Date
JP2008538399A JP2008538399A (ja) 2008-10-23
JP2008538399A5 JP2008538399A5 (enExample) 2009-03-12
JP4874329B2 true JP4874329B2 (ja) 2012-02-15

Family

ID=34935569

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008507029A Expired - Fee Related JP4874329B2 (ja) 2005-04-21 2006-01-20 カバープレートとこのカバープレートに被着された保護層とを備えたタービン翼

Country Status (5)

Country Link
US (1) US8021120B2 (enExample)
EP (2) EP1715140A1 (enExample)
JP (1) JP4874329B2 (enExample)
CN (1) CN101163862B (enExample)
WO (1) WO2006111427A1 (enExample)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8708658B2 (en) * 2007-04-12 2014-04-29 United Technologies Corporation Local application of a protective coating on a shrouded gas turbine engine component
KR101115761B1 (ko) * 2008-12-26 2012-06-12 주식회사 포스코 표면 탈탄이 억제된 강재 및 제조방법
DE102010049398A1 (de) * 2009-11-02 2011-05-05 Alstom Technology Ltd. Verschleiss- und oxidationsbeständige Turbinenschaufel
CN101922312B (zh) * 2010-03-24 2013-11-06 北京航空航天大学 一种叶轮机械径向间隙泄漏损失的控制方法
US8579581B2 (en) * 2010-09-15 2013-11-12 General Electric Company Abradable bucket shroud
US8753093B2 (en) * 2010-10-19 2014-06-17 General Electric Company Bonded turbine bucket tip shroud and related method
EP2549063A1 (en) * 2011-07-21 2013-01-23 Siemens Aktiengesellschaft Heat shield element for a gas turbine
US20130034423A1 (en) * 2011-08-01 2013-02-07 General Electric Company System and method for passively controlling clearance in a gas turbine engine
CN104508251B (zh) * 2012-04-27 2016-08-24 通用电气公司 用于燃气涡轮发动机的护罩组件和密封件
RU2015117053A (ru) * 2012-11-06 2016-12-27 Сименс Энерджи, Инк. Венец лопатки турбины с абразивным покрытием
DE102013212252A1 (de) * 2013-06-26 2014-12-31 Siemens Aktiengesellschaft Turbine und Verfahren zur Anstreiferkennung
US20150093237A1 (en) * 2013-09-30 2015-04-02 General Electric Company Ceramic matrix composite component, turbine system and fabrication process
GB2521588A (en) * 2013-10-11 2015-07-01 Reaction Engines Ltd Turbine blades
WO2015068227A1 (ja) * 2013-11-06 2015-05-14 川崎重工業株式会社 タービン翼およびその製造方法
DE102014202457A1 (de) 2014-02-11 2015-08-13 Siemens Aktiengesellschaft Verbesserte Verschleißbeständigkeit eines Hochtemperaturbauteils durch Kobaltbeschichtung
US10662788B2 (en) * 2018-02-02 2020-05-26 Raytheon Technologies Corporation Wear resistant turbine blade tip
US11203942B2 (en) 2018-03-14 2021-12-21 Raytheon Technologies Corporation Wear resistant airfoil tip
US11346232B2 (en) * 2018-04-23 2022-05-31 Rolls-Royce Corporation Turbine blade with abradable tip
FR3090427B1 (fr) * 2018-12-21 2023-11-10 Safran Procede de fabrication d’un noyau
WO2022107734A1 (ja) * 2020-11-20 2022-05-27 川崎重工業株式会社 ガスタービンエンジンの回転部構成部材およびその製造方法
WO2023202900A1 (de) * 2022-04-21 2023-10-26 Siemens Energy Global GmbH & Co. KG Dichtungsanordnung

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4913810B1 (enExample) * 1965-02-24 1974-04-03
JPH0219603A (ja) * 1988-07-07 1990-01-23 Union Carbide Corp 回転式ラビリンスシール部材用耐摩耗性、研削性レーザ彫刻セラミック乃至金属炭化物表面
JP2002256449A (ja) * 2001-02-28 2002-09-11 Mitsubishi Heavy Ind Ltd 耐摩耗性コーティング及びその施工方法
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
JP2003532014A (ja) * 2000-05-04 2003-10-28 シーメンス アクチエンゲゼルシヤフト 隙間の漏止め装置

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE676992A (enExample) * 1965-02-24 1966-07-18
FI45933C (fi) 1972-03-22 1976-12-03 Salakarin Oikeudenomistajat Liukumista estävä laite pyörää ja sentapaista varten.
US4291448A (en) * 1977-12-12 1981-09-29 Turbine Components Corporation Method of restoring the shrouds of turbine blades
US4285108A (en) * 1979-02-23 1981-08-25 United Technologies Corporation Apparatus and method for refinishing turbine blade airseals
US4822248A (en) * 1987-04-15 1989-04-18 Metallurgical Industries, Inc. Rebuilt shrouded turbine blade and method of rebuilding the same
US5358379A (en) * 1993-10-27 1994-10-25 Westinghouse Electric Corporation Gas turbine vane
DE10140742B4 (de) * 2000-12-16 2015-02-12 Alstom Technology Ltd. Vorrichtung zur Dichtspaltreduzierung zwischen einer rotierenden und einer stationären Komponente innerhalb einer axial durchströmten Strömungsmaschine
JP3902179B2 (ja) * 2001-05-31 2007-04-04 三菱重工業株式会社 皮膜形成方法及び皮膜形成用材料、並びに研磨性皮膜形成用シート
KR101004236B1 (ko) * 2002-10-09 2010-12-24 미츠비시덴키 가부시키가이샤 회전체 및 그 코팅방법

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4913810B1 (enExample) * 1965-02-24 1974-04-03
JPH0219603A (ja) * 1988-07-07 1990-01-23 Union Carbide Corp 回転式ラビリンスシール部材用耐摩耗性、研削性レーザ彫刻セラミック乃至金属炭化物表面
JP2003532014A (ja) * 2000-05-04 2003-10-28 シーメンス アクチエンゲゼルシヤフト 隙間の漏止め装置
JP2002256449A (ja) * 2001-02-28 2002-09-11 Mitsubishi Heavy Ind Ltd 耐摩耗性コーティング及びその施工方法
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

Also Published As

Publication number Publication date
US8021120B2 (en) 2011-09-20
WO2006111427A1 (de) 2006-10-26
EP1871991A1 (de) 2008-01-02
EP1715140A1 (de) 2006-10-25
US20090022583A1 (en) 2009-01-22
CN101163862A (zh) 2008-04-16
JP2008538399A (ja) 2008-10-23
CN101163862B (zh) 2011-10-05

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