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 PDFInfo
- 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
- Authority
- CN
- China
- Prior art keywords
- airfoil
- platform
- dovetail
- dovetail type
- pottery
- 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.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3084—Fixing blades to rotors; Blade roots ; Blade spacers the blades being made of ceramics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
- F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/284—Selection of ceramic materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
- F05D2300/6033—Ceramic matrix composites [CMC]
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite 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)
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)
| 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)
| 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 |
-
2012
- 2012-01-03 US US13/342,599 patent/US8967974B2/en active Active
- 2012-10-30 JP JP2012238468A patent/JP6043154B2/ja active Active
- 2012-10-31 EP EP12190922.0A patent/EP2612997B1/en not_active Revoked
- 2012-11-02 CN CN201210432509.4A patent/CN103184890B/zh active Active
- 2012-11-02 RU RU2012146619/06A patent/RU2012146619A/ru not_active Application Discontinuation
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 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103184890B (zh) | 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 | |
| CN102213108B (zh) | 复合型涡轮轮叶组件 | |
| CN102678188B (zh) | 涡轮叶片组件 | |
| JP6145167B2 (ja) | セラミック基材料を含有する翼形部品及びその方法 | |
| US7931442B1 (en) | Rotor blade assembly with de-coupled composite platform | |
| JP5976311B2 (ja) | セラミック基材料を含むタービンエアフォイル部品とその製造工程 | |
| US8142163B1 (en) | Turbine blade with spar and shell | |
| US7147440B2 (en) | Methods and apparatus for cooling gas turbine engine rotor assemblies | |
| JP5970182B2 (ja) | セラミック基材料と金属材料とから成る部品の製造工程 | |
| CN100359134C (zh) | 根部开有缺口的涡轮叶片 | |
| EP2204544B1 (en) | Non-integral turbine blade platform, corresponding turbine blade assembly and assembling method | |
| US7874804B1 (en) | Turbine blade with detached platform | |
| JP4731238B2 (ja) | ガスタービンエンジンロータブレードを冷却するための装置 | |
| CN102953764B (zh) | 连接的叶片平台以及密封方法 | |
| JP6240388B2 (ja) | 中空cmcバケット用の薄肉強化格子構造体 | |
| US20120034101A1 (en) | Turbine blade squealer tip | |
| JP6457500B2 (ja) | ターボ機械用ロータリアセンブリ | |
| JP2005133726A (ja) | ガスタービンエンジンロータ組立体を冷却するための方法及び装置 | |
| JP2009024698A (ja) | 押付けプレートシール | |
| EP2578807A2 (en) | Airfoil for turbine system | |
| JP2007537384A (ja) | ブレードの固定軽減不整合 | |
| CN114585802A (zh) | 涡轮叶片、制造涡轮叶片的方法和整修涡轮叶片的方法 | |
| US10767496B2 (en) | Turbine blade assembly with mounted platform | |
| US20090202344A1 (en) | Rotating assembly for a turbomachine | |
| CN101845970A (zh) | 涡轮机转子组件和方法 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| 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 |