CN103184890B - 复合叶片组件及包括该组件的涡轮转子叶轮及装配陶瓷翼型件的方法 - Google Patents

复合叶片组件及包括该组件的涡轮转子叶轮及装配陶瓷翼型件的方法 Download PDF

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Publication number
CN103184890B
CN103184890B CN201210432509.4A CN201210432509A CN103184890B CN 103184890 B CN103184890 B CN 103184890B CN 201210432509 A CN201210432509 A CN 201210432509A CN 103184890 B CN103184890 B CN 103184890B
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China
Prior art keywords
airfoil
platform
dovetail
dovetail type
pottery
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Active
Application number
CN201210432509.4A
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English (en)
Chinese (zh)
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CN103184890A (zh
Inventor
A.J.加西亚-克雷斯波
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General Electric Company PLC
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General Electric Co
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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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3084Fixing blades to rotors; Blade roots ; Blade spacers the blades being made of ceramics
    • 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
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • F01D11/008Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • 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
    • F01D5/284Selection of ceramic materials
    • 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
    • F05D2300/603Composites; e.g. fibre-reinforced
    • F05D2300/6033Ceramic matrix composites [CMC]
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • 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
    • 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
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
    • 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
    • Y10T29/49336Blade making
    • Y10T29/49337Composite blade

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201210432509.4A 2012-01-03 2012-11-02 复合叶片组件及包括该组件的涡轮转子叶轮及装配陶瓷翼型件的方法 Active CN103184890B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/342,599 US8967974B2 (en) 2012-01-03 2012-01-03 Composite airfoil assembly
US13/342599 2012-01-03

Publications (2)

Publication Number Publication Date
CN103184890A CN103184890A (zh) 2013-07-03
CN103184890B true CN103184890B (zh) 2016-11-23

Family

ID=47143658

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210432509.4A Active CN103184890B (zh) 2012-01-03 2012-11-02 复合叶片组件及包括该组件的涡轮转子叶轮及装配陶瓷翼型件的方法

Country Status (5)

Country Link
US (1) US8967974B2 (2)
EP (1) EP2612997B1 (2)
JP (1) JP6043154B2 (2)
CN (1) CN103184890B (2)
RU (1) RU2012146619A (2)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9353629B2 (en) * 2012-11-30 2016-05-31 Solar Turbines Incorporated Turbine blade apparatus
EP2762679A1 (en) * 2013-02-01 2014-08-06 Siemens Aktiengesellschaft Gas Turbine Rotor Blade and Gas Turbine Rotor
US9453422B2 (en) 2013-03-08 2016-09-27 General Electric Company Device, system and method for preventing leakage in a turbine
US9482108B2 (en) * 2013-04-03 2016-11-01 General Electric Company Turbomachine blade assembly
US20150003997A1 (en) * 2013-07-01 2015-01-01 United Technologies Corporation Method of forming hybrid metal ceramic components
EP3052763B1 (en) * 2013-09-30 2020-07-15 United Technologies Corporation A nonmetallic airfoil with a compliant attachment
EP3055509B1 (en) * 2013-10-11 2024-03-06 RTX Corporation Ceramic matrix composite gas turbine blade with monolithic ceramic platform and dovetail
US9969654B2 (en) 2014-01-24 2018-05-15 United Technologies Corporation Method of bonding a metallic component to a non-metallic component using a compliant material
CN104454230A (zh) * 2014-10-21 2015-03-25 西北工业大学 一种大气相变发动机叶片及控制方法
US10253639B2 (en) * 2015-02-05 2019-04-09 Rolls-Royce North American Technologies, Inc. Ceramic matrix composite gas turbine engine blade
US10358922B2 (en) 2016-11-10 2019-07-23 Rolls-Royce Corporation Turbine wheel with circumferentially-installed inter-blade heat shields
US10648354B2 (en) 2016-12-02 2020-05-12 Honeywell International Inc. Turbine wheels, turbine engines including the same, and methods of forming turbine wheels with improved seal plate sealing
US10494934B2 (en) * 2017-02-14 2019-12-03 General Electric Company Turbine blades having shank features
US10683765B2 (en) 2017-02-14 2020-06-16 General Electric Company Turbine blades having shank features and methods of fabricating the same
US10731487B2 (en) 2017-02-20 2020-08-04 General Electric Company Turbine components and methods of manufacturing
EP3438410B1 (en) 2017-08-01 2021-09-29 General Electric Company Sealing system for a rotary machine
US10975714B2 (en) 2018-11-22 2021-04-13 Pratt & Whitney Canada Corp. Rotor assembly with blade sealing tab
CN110700898B (zh) * 2019-11-21 2025-08-26 中国科学院工程热物理研究所 陶瓷-金属相结合的透平导向叶片及其燃气轮机
US11441430B2 (en) * 2020-02-07 2022-09-13 Raytheon Technologies Corporation Airfoil with buffer layer to absorb thermal mismatch
KR102436365B1 (ko) * 2020-08-04 2022-08-25 태형물산 주식회사 반려동물용 사료 자동 공급기
CN114536792B (zh) * 2022-04-27 2022-08-12 北京玻钢院复合材料有限公司 一种复合材料部件与金属部件的连接结构及连接方法
CN115585019B (zh) * 2022-08-29 2025-06-17 中国航发四川燃气涡轮研究院 组合式陶瓷基复合材料双层壁高压涡轮转子叶片
US12410715B2 (en) 2023-08-10 2025-09-09 General Electric Company Rotor blade system for turbine engines
US12410720B2 (en) 2023-11-02 2025-09-09 General Electric Company Turbine engine having a rotatable disk and a blade

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3801222A (en) * 1972-02-28 1974-04-02 United Aircraft Corp Platform for compressor or fan blade
JPH0571305A (ja) * 1991-03-04 1993-03-23 General Electric Co <Ge> ロータブレードをロータデイスクに取付けるプラツトホームアセンブリ
US5222865A (en) 1991-03-04 1993-06-29 General Electric Company Platform assembly for attaching rotor blades to a rotor disk
FR2697285B1 (fr) * 1992-10-28 1994-11-25 Snecma Système de verrouillage d'extrémités d'aubes.
US5720597A (en) 1996-01-29 1998-02-24 General Electric Company Multi-component blade for a gas turbine
JPH1054204A (ja) 1996-05-20 1998-02-24 General Electric Co <Ge> ガスタービン用の多構成部翼
US6200092B1 (en) * 1999-09-24 2001-03-13 General Electric Company Ceramic turbine nozzle
US6325593B1 (en) 2000-02-18 2001-12-04 General Electric Company Ceramic turbine airfoils with cooled trailing edge blocks
US6553665B2 (en) 2000-03-08 2003-04-29 General Electric Company Stator vane assembly for a turbine and method for forming the assembly
US6441341B1 (en) 2000-06-16 2002-08-27 General Electric Company Method of forming cooling holes in a ceramic matrix composite turbine components
US6648596B1 (en) 2000-11-08 2003-11-18 General Electric Company Turbine blade or turbine vane made of a ceramic foam joined to a metallic nonfoam, and preparation thereof
US6447250B1 (en) * 2000-11-27 2002-09-10 General Electric Company Non-integral fan platform
US6610385B2 (en) 2001-12-20 2003-08-26 General Electric Company Integral surface features for CMC components and method therefor
US6866897B2 (en) * 2002-09-30 2005-03-15 General Electric Company Method for manufacturing articles for high temperature use, and articles made therewith
US6915840B2 (en) 2002-12-17 2005-07-12 General Electric Company Methods and apparatus for fabricating turbine engine airfoils
US7284958B2 (en) * 2003-03-22 2007-10-23 Allison Advanced Development Company Separable blade platform
US7044709B2 (en) 2004-01-15 2006-05-16 General Electric Company Methods and apparatus for coupling ceramic matrix composite turbine components
US7510379B2 (en) 2005-12-22 2009-03-31 General Electric Company Composite blading member and method for making
US7766623B2 (en) 2006-11-08 2010-08-03 General Electric Company System for manufacturing a rotor having an MMC ring component and an airfoil component having monolithic airfoils
US7874804B1 (en) 2007-05-10 2011-01-25 Florida Turbine Technologies, Inc. Turbine blade with detached platform
CH700071A1 (de) * 2008-12-12 2010-06-15 Alstom Technology Ltd Laufschaufel für eine Gasturbine.
US8496443B2 (en) 2009-12-15 2013-07-30 Siemens Energy, Inc. Modular turbine airfoil and platform assembly with independent root teeth
US8231354B2 (en) 2009-12-15 2012-07-31 Siemens Energy, Inc. Turbine engine airfoil and platform assembly
US8727730B2 (en) * 2010-04-06 2014-05-20 General Electric Company Composite turbine bucket assembly
US8721290B2 (en) 2010-12-23 2014-05-13 General Electric Company Processes for producing components containing ceramic-based and metallic materials

Also Published As

Publication number Publication date
JP6043154B2 (ja) 2016-12-14
JP2013139765A (ja) 2013-07-18
EP2612997B1 (en) 2017-04-26
US20130171001A1 (en) 2013-07-04
CN103184890A (zh) 2013-07-03
EP2612997A2 (en) 2013-07-10
US8967974B2 (en) 2015-03-03
EP2612997A3 (en) 2014-03-12
RU2012146619A (ru) 2014-05-10

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
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GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20231226

Address after: Swiss Baden

Patentee after: GENERAL ELECTRIC CO. LTD.

Address before: New York State, USA

Patentee before: General Electric Co.

TR01 Transfer of patent right