JP2015512486A - プラットフォームを有するモジュール式タービン翼 - Google Patents
プラットフォームを有するモジュール式タービン翼 Download PDFInfo
- Publication number
- JP2015512486A JP2015512486A JP2015502347A JP2015502347A JP2015512486A JP 2015512486 A JP2015512486 A JP 2015512486A JP 2015502347 A JP2015502347 A JP 2015502347A JP 2015502347 A JP2015502347 A JP 2015502347A JP 2015512486 A JP2015512486 A JP 2015512486A
- Authority
- JP
- Japan
- Prior art keywords
- platform
- blade
- turbine blade
- turbine
- extension
- 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.)
- Pending
Links
Images
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
-
- 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
- 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
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/80—Platforms for stationary or moving blades
-
- 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
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP12162106.4A EP2644828A1 (de) | 2012-03-29 | 2012-03-29 | Modulare Turbinenschaufel mit Plattform |
EP12162106.4 | 2012-03-29 | ||
PCT/EP2013/056652 WO2013144270A1 (de) | 2012-03-29 | 2013-03-28 | Modulare turbinenschaufel mit plattform |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2015512486A true JP2015512486A (ja) | 2015-04-27 |
Family
ID=48045499
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2015502347A Pending JP2015512486A (ja) | 2012-03-29 | 2013-03-28 | プラットフォームを有するモジュール式タービン翼 |
Country Status (6)
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107075952A (zh) * | 2014-10-28 | 2017-08-18 | 西门子能源公司 | 模块化涡轮叶片 |
US10934870B2 (en) | 2018-09-17 | 2021-03-02 | Rolls Royce Plc | Turbine vane assembly with reinforced end wall joints |
CN110132556B (zh) * | 2019-04-30 | 2021-11-12 | 中国航发湖南动力机械研究所 | 模块化涡轮试验件及其试验方法 |
DE102020201448A1 (de) * | 2020-02-06 | 2021-08-12 | Siemens Aktiengesellschaft | Additiv hergestellte Turbinenschaufel mit Verdrehsicherung und Justageverfahren |
US11834960B2 (en) * | 2022-02-18 | 2023-12-05 | General Electric Company | Methods and apparatus to reduce deflection of an airfoil |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3451654A (en) * | 1967-08-25 | 1969-06-24 | Gen Motors Corp | Blade vibration damping |
US4501053A (en) * | 1982-06-14 | 1985-02-26 | United Technologies Corporation | Method of making rotor blade for a rotary machine |
JPS6238801A (ja) * | 1985-08-12 | 1987-02-19 | Mitsubishi Heavy Ind Ltd | 組立式タ−ビン動翼 |
JPS6241902A (ja) * | 1985-08-15 | 1987-02-23 | Hitachi Ltd | ガスタ−ビン用動翼構造 |
US5083900A (en) * | 1989-11-15 | 1992-01-28 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Turbomachine stator element |
JPH04252806A (ja) * | 1990-08-15 | 1992-09-08 | Tokyo Electric Power Co Inc:The | ガスタービンの静翼 |
US20100054932A1 (en) * | 2008-09-03 | 2010-03-04 | Siemens Power Generation, Inc. | Circumferential Shroud Inserts for a Gas Turbine Vane Platform |
US20100150703A1 (en) * | 2006-09-22 | 2010-06-17 | Siemens Power Generation, Inc. | Stacked laminate bolted ring segment |
US20100189556A1 (en) * | 2009-01-28 | 2010-07-29 | United Technologies Corporation | Segmented ceramic matrix composite turbine airfoil component |
US20110142639A1 (en) * | 2009-12-15 | 2011-06-16 | Campbell Christian X | Modular turbine airfoil and platform assembly with independent root teeth |
EP2374999A2 (en) * | 2010-04-06 | 2011-10-12 | General Electric Company | Composite turbine bucket assembly |
Family Cites Families (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE470026A (enrdf_load_stackoverflow) * | 1945-12-21 | |||
US3801222A (en) * | 1972-02-28 | 1974-04-02 | United Aircraft Corp | Platform for compressor or fan blade |
US3749518A (en) * | 1972-03-15 | 1973-07-31 | United Aircraft Corp | Composite blade root configuration |
US3778185A (en) * | 1972-08-28 | 1973-12-11 | United Aircraft Corp | Composite strut joint construction |
US4152816A (en) * | 1977-06-06 | 1979-05-08 | General Motors Corporation | Method of manufacturing a hybrid turbine rotor |
FR2463849A1 (fr) * | 1979-08-23 | 1981-02-27 | Onera (Off Nat Aerospatiale) | Perfectionnements apportes aux aubes tournantes de turbines a gaz, et aux turbines a gaz equipees de ces aubes |
US4583914A (en) * | 1982-06-14 | 1986-04-22 | United Technologies Corp. | Rotor blade for a rotary machine |
US4650399A (en) * | 1982-06-14 | 1987-03-17 | United Technologies Corporation | Rotor blade for a rotary machine |
US5318406A (en) * | 1992-11-02 | 1994-06-07 | General Electric Company | Multipart gas turbine blade |
WO2000057032A1 (de) * | 1999-03-24 | 2000-09-28 | Siemens Aktiengesellschaft | Leitschaufel und leitschaufelkranz für eine strömungsmaschine, sowie bauteil zur begrenzung eines strömungskanals |
EP1219787B1 (de) * | 2000-12-27 | 2005-12-21 | Siemens Aktiengesellschaft | Gasturbinenschaufel und Gasturbine |
US6648597B1 (en) * | 2002-05-31 | 2003-11-18 | Siemens Westinghouse Power Corporation | Ceramic matrix composite turbine vane |
US7284958B2 (en) * | 2003-03-22 | 2007-10-23 | Allison Advanced Development Company | Separable blade platform |
DE10346240A1 (de) * | 2003-10-06 | 2005-04-21 | Alstom Technology Ltd Baden | Bauteil einer Gasturbine |
JP4860941B2 (ja) * | 2005-04-27 | 2012-01-25 | 本田技研工業株式会社 | 整流部材ユニット及びその製造方法 |
US7604456B2 (en) * | 2006-04-11 | 2009-10-20 | Siemens Energy, Inc. | Vane shroud through-flow platform cover |
US7581924B2 (en) * | 2006-07-27 | 2009-09-01 | Siemens Energy, Inc. | Turbine vanes with airfoil-proximate cooling seam |
US7972113B1 (en) * | 2007-05-02 | 2011-07-05 | Florida Turbine Technologies, Inc. | Integral turbine blade and platform |
US7874804B1 (en) * | 2007-05-10 | 2011-01-25 | Florida Turbine Technologies, Inc. | Turbine blade with detached platform |
US7976281B2 (en) * | 2007-05-15 | 2011-07-12 | General Electric Company | Turbine rotor blade and method of assembling the same |
US20080298973A1 (en) * | 2007-05-29 | 2008-12-04 | Siemens Power Generation, Inc. | Turbine vane with divided turbine vane platform |
US8162617B1 (en) * | 2008-01-30 | 2012-04-24 | Florida Turbine Technologies, Inc. | Turbine blade with spar and shell |
US8408874B2 (en) * | 2008-04-11 | 2013-04-02 | United Technologies Corporation | Platformless turbine blade |
US8033790B2 (en) * | 2008-09-26 | 2011-10-11 | Siemens Energy, Inc. | Multiple piece turbine engine airfoil with a structural spar |
US8714932B2 (en) * | 2008-12-31 | 2014-05-06 | General Electric Company | Ceramic matrix composite blade having integral platform structures and methods of fabrication |
US8231354B2 (en) * | 2009-12-15 | 2012-07-31 | Siemens Energy, Inc. | Turbine engine airfoil and platform assembly |
US8914976B2 (en) * | 2010-04-01 | 2014-12-23 | Siemens Energy, Inc. | Turbine airfoil to shroud attachment method |
EP2644834A1 (de) * | 2012-03-29 | 2013-10-02 | Siemens Aktiengesellschaft | Turbinenschaufel sowie zugehöriges Verfahren zum Herstellen einer Turbinenschaufel |
-
2012
- 2012-03-29 EP EP12162106.4A patent/EP2644828A1/de not_active Withdrawn
-
2013
- 2013-03-28 WO PCT/EP2013/056652 patent/WO2013144270A1/de active Application Filing
- 2013-03-28 EP EP13713848.3A patent/EP2807342A1/de not_active Withdrawn
- 2013-03-28 US US14/388,458 patent/US20150071783A1/en not_active Abandoned
- 2013-03-28 CN CN201380017983.3A patent/CN104220700A/zh active Pending
- 2013-03-28 JP JP2015502347A patent/JP2015512486A/ja active Pending
- 2013-03-28 IN IN7525DEN2014 patent/IN2014DN07525A/en unknown
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3451654A (en) * | 1967-08-25 | 1969-06-24 | Gen Motors Corp | Blade vibration damping |
US4501053A (en) * | 1982-06-14 | 1985-02-26 | United Technologies Corporation | Method of making rotor blade for a rotary machine |
JPS6238801A (ja) * | 1985-08-12 | 1987-02-19 | Mitsubishi Heavy Ind Ltd | 組立式タ−ビン動翼 |
JPS6241902A (ja) * | 1985-08-15 | 1987-02-23 | Hitachi Ltd | ガスタ−ビン用動翼構造 |
US5083900A (en) * | 1989-11-15 | 1992-01-28 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Turbomachine stator element |
JPH04252806A (ja) * | 1990-08-15 | 1992-09-08 | Tokyo Electric Power Co Inc:The | ガスタービンの静翼 |
US20100150703A1 (en) * | 2006-09-22 | 2010-06-17 | Siemens Power Generation, Inc. | Stacked laminate bolted ring segment |
US20100054932A1 (en) * | 2008-09-03 | 2010-03-04 | Siemens Power Generation, Inc. | Circumferential Shroud Inserts for a Gas Turbine Vane Platform |
US20100189556A1 (en) * | 2009-01-28 | 2010-07-29 | United Technologies Corporation | Segmented ceramic matrix composite turbine airfoil component |
US20110142639A1 (en) * | 2009-12-15 | 2011-06-16 | Campbell Christian X | Modular turbine airfoil and platform assembly with independent root teeth |
EP2374999A2 (en) * | 2010-04-06 | 2011-10-12 | General Electric Company | Composite turbine bucket assembly |
JP2011220325A (ja) * | 2010-04-06 | 2011-11-04 | General Electric Co <Ge> | 複合タービン動翼組立体 |
Also Published As
Publication number | Publication date |
---|---|
WO2013144270A1 (de) | 2013-10-03 |
EP2644828A1 (de) | 2013-10-02 |
US20150071783A1 (en) | 2015-03-12 |
EP2807342A1 (de) | 2014-12-03 |
IN2014DN07525A (enrdf_load_stackoverflow) | 2015-04-24 |
CN104220700A (zh) | 2014-12-17 |
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Legal Events
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A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20150220 |
|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20150220 |
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A977 | Report on retrieval |
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A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20160307 |
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A02 | Decision of refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A02 Effective date: 20161024 |