DE59810315D1 - Turbinenschaufel einer Gasturbine - Google Patents
Turbinenschaufel einer GasturbineInfo
- Publication number
- DE59810315D1 DE59810315D1 DE59810315T DE59810315T DE59810315D1 DE 59810315 D1 DE59810315 D1 DE 59810315D1 DE 59810315 T DE59810315 T DE 59810315T DE 59810315 T DE59810315 T DE 59810315T DE 59810315 D1 DE59810315 D1 DE 59810315D1
- Authority
- DE
- Germany
- Prior art keywords
- turbine
- blade
- gas
- gas turbine
- turbine blade
- 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 - Lifetime
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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19738065A DE19738065A1 (de) | 1997-09-01 | 1997-09-01 | Turbinenschaufel einer Gasturbine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE59810315D1 true DE59810315D1 (de) | 2004-01-15 |
Family
ID=7840791
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19738065A Ceased DE19738065A1 (de) | 1997-09-01 | 1997-09-01 | Turbinenschaufel einer Gasturbine |
DE59810315T Expired - Lifetime DE59810315D1 (de) | 1997-09-01 | 1998-08-11 | Turbinenschaufel einer Gasturbine |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19738065A Ceased DE19738065A1 (de) | 1997-09-01 | 1997-09-01 | Turbinenschaufel einer Gasturbine |
Country Status (5)
Country | Link |
---|---|
US (1) | US6033181A (de) |
EP (1) | EP0899425B1 (de) |
JP (1) | JPH11132003A (de) |
CN (1) | CN1120287C (de) |
DE (2) | DE19738065A1 (de) |
Families Citing this family (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1342882B1 (de) * | 1998-12-10 | 2006-05-17 | ALSTOM Technology Ltd | Verfahren zur Herstellung eines geschweissten Rotors einer Strömungsmaschine |
DE19902437C5 (de) | 1999-01-22 | 2017-01-12 | General Electric Technology Gmbh | Verfahren und Vorrichtung zum schnellen Anfahren und zur schnellen Leistungssteigerung einer Gasturbinenanlage |
DE10027842A1 (de) | 2000-06-05 | 2001-12-20 | Alstom Power Nv | Verfahren zum Kühlen einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens |
DE10027833A1 (de) | 2000-06-05 | 2001-12-13 | Alstom Power Nv | Verfahren zum Kühlen einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens |
GB0025012D0 (en) * | 2000-10-12 | 2000-11-29 | Rolls Royce Plc | Cooling of gas turbine engine aerofoils |
DE10053356A1 (de) * | 2000-10-27 | 2002-05-08 | Alstom Switzerland Ltd | Gekühltes Bauteil, Gusskern für die Herstellung eines solchen Bauteils, sowie Verfahren zum Herstellen eines solchen Bauteils |
EP1321627A1 (de) * | 2001-12-21 | 2003-06-25 | Siemens Aktiengesellschaft | Luft- und dampfgekühlte Turbinenschaufel und ein Verfahren zum Kühlen einer Turbinenschaufel |
JP2003200936A (ja) * | 2001-12-28 | 2003-07-15 | Toyo Roki Mfg Co Ltd | 容器の水抜き穴形状 |
US6932573B2 (en) * | 2003-04-30 | 2005-08-23 | Siemens Westinghouse Power Corporation | Turbine blade having a vortex forming cooling system for a trailing edge |
US7195448B2 (en) * | 2004-05-27 | 2007-03-27 | United Technologies Corporation | Cooled rotor blade |
US20050265839A1 (en) | 2004-05-27 | 2005-12-01 | United Technologies Corporation | Cooled rotor blade |
US7198468B2 (en) * | 2004-07-15 | 2007-04-03 | Pratt & Whitney Canada Corp. | Internally cooled turbine blade |
US7097419B2 (en) * | 2004-07-26 | 2006-08-29 | General Electric Company | Common tip chamber blade |
EP1621730B1 (de) | 2004-07-26 | 2008-10-08 | Siemens Aktiengesellschaft | Gekühltes Bauteil einer Strömungsmaschine und Verfahren zum Giessen dieses gekühlten Bauteils |
GB0418914D0 (en) * | 2004-08-25 | 2004-09-29 | Rolls Royce Plc | Turbine component |
US7128533B2 (en) * | 2004-09-10 | 2006-10-31 | Siemens Power Generation, Inc. | Vortex cooling system for a turbine blade |
US7217097B2 (en) * | 2005-01-07 | 2007-05-15 | Siemens Power Generation, Inc. | Cooling system with internal flow guide within a turbine blade of a turbine engine |
US7189060B2 (en) * | 2005-01-07 | 2007-03-13 | Siemens Power Generation, Inc. | Cooling system including mini channels within a turbine blade of a turbine engine |
US7632071B2 (en) * | 2005-12-15 | 2009-12-15 | United Technologies Corporation | Cooled turbine blade |
WO2009016744A1 (ja) * | 2007-07-31 | 2009-02-05 | Mitsubishi Heavy Industries, Ltd. | タービン用翼 |
US8376706B2 (en) * | 2007-09-28 | 2013-02-19 | General Electric Company | Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method |
US10286407B2 (en) | 2007-11-29 | 2019-05-14 | General Electric Company | Inertial separator |
US8393157B2 (en) * | 2008-01-18 | 2013-03-12 | General Electric Company | Swozzle design for gas turbine combustor |
US8511968B2 (en) * | 2009-08-13 | 2013-08-20 | Siemens Energy, Inc. | Turbine vane for a gas turbine engine having serpentine cooling channels with internal flow blockers |
DE102010046331A1 (de) * | 2010-09-23 | 2012-03-29 | Rolls-Royce Deutschland Ltd & Co Kg | Gekühlte Turbinenschaufeln für ein Gasturbinentriebwerk |
CH705181A1 (de) | 2011-06-16 | 2012-12-31 | Alstom Technology Ltd | Verfahren zum Kühlen einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens. |
US8840370B2 (en) | 2011-11-04 | 2014-09-23 | General Electric Company | Bucket assembly for turbine system |
JP6169161B2 (ja) | 2012-03-22 | 2017-07-26 | ゼネラル エレクトリック テクノロジー ゲゼルシャフト ミット ベシュレンクテル ハフツングGeneral Electric Technology GmbH | タービン翼 |
CN103806951A (zh) * | 2014-01-20 | 2014-05-21 | 北京航空航天大学 | 一种缝气膜冷却加扰流柱的组合式涡轮叶片 |
WO2016032585A2 (en) | 2014-05-29 | 2016-03-03 | General Electric Company | Turbine engine, components, and methods of cooling same |
US11033845B2 (en) | 2014-05-29 | 2021-06-15 | General Electric Company | Turbine engine and particle separators therefore |
US9915176B2 (en) | 2014-05-29 | 2018-03-13 | General Electric Company | Shroud assembly for turbine engine |
WO2016025056A2 (en) | 2014-05-29 | 2016-02-18 | General Electric Company | Turbine engine and particle separators therefore |
US10036319B2 (en) | 2014-10-31 | 2018-07-31 | General Electric Company | Separator assembly for a gas turbine engine |
US10167725B2 (en) | 2014-10-31 | 2019-01-01 | General Electric Company | Engine component for a turbine engine |
CN104696018B (zh) * | 2015-02-15 | 2016-02-17 | 德清透平机械制造有限公司 | 一种高效汽轮机叶片 |
US10428664B2 (en) | 2015-10-15 | 2019-10-01 | General Electric Company | Nozzle for a gas turbine engine |
US9988936B2 (en) | 2015-10-15 | 2018-06-05 | General Electric Company | Shroud assembly for a gas turbine engine |
US10174620B2 (en) | 2015-10-15 | 2019-01-08 | General Electric Company | Turbine blade |
CN105840315B (zh) * | 2016-03-15 | 2017-10-31 | 哈尔滨工程大学 | 一种应用于气膜冷却技术的旋流冷气腔结构 |
CN105909318B (zh) * | 2016-04-26 | 2017-09-26 | 西北工业大学 | 一种用于涡轮叶片气膜冷却出口上游扩张孔结构 |
US10704425B2 (en) | 2016-07-14 | 2020-07-07 | General Electric Company | Assembly for a gas turbine engine |
FR3062675B1 (fr) * | 2017-02-07 | 2021-01-15 | Safran Helicopter Engines | Aube haute pression ventilee de turbine d'helicoptere comprenant un conduit amont et une cavite centrale de refroidissement |
US10801724B2 (en) * | 2017-06-14 | 2020-10-13 | General Electric Company | Method and apparatus for minimizing cross-flow across an engine cooling hole |
EP3425165B1 (de) * | 2017-07-05 | 2022-08-31 | General Electric Technology GmbH | Mechanische komponente |
CN109812301A (zh) * | 2019-03-06 | 2019-05-28 | 上海交通大学 | 一种具有横向通气孔的涡轮叶片双层壁冷却结构 |
CN112483191B (zh) * | 2020-11-30 | 2022-07-19 | 日照黎阳工业装备有限公司 | 一种适用于燃气轮机具备对流换热功能的涡轮叶片 |
CN115234306A (zh) * | 2022-09-21 | 2022-10-25 | 中国航发燃气轮机有限公司 | 一种燃气轮机透平气冷叶片 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB856983A (en) * | 1958-06-18 | 1960-12-21 | Rolls Royce | Improvements in the formation of holes by spark erosion |
FR90542E (fr) * | 1965-08-02 | 1967-12-29 | Snecma | Perfectionnement aux moyens de refroidissement d'aubes de turbine ou autres pièces |
US4565490A (en) * | 1981-06-17 | 1986-01-21 | Rice Ivan G | Integrated gas/steam nozzle |
DE3211139C1 (de) * | 1982-03-26 | 1983-08-11 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Axialturbinenschaufel,insbesondere Axialturbinenlaufschaufel fuer Gasturbinentriebwerke |
US4770608A (en) | 1985-12-23 | 1988-09-13 | United Technologies Corporation | Film cooled vanes and turbines |
JPS62294703A (ja) * | 1986-06-13 | 1987-12-22 | Jinichi Nishiwaki | 蒸気タ−ビンのブレ−ドを冷却する方法 |
GB2202907A (en) * | 1987-03-26 | 1988-10-05 | Secr Defence | Cooled aerofoil components |
US5253976A (en) * | 1991-11-19 | 1993-10-19 | General Electric Company | Integrated steam and air cooling for combined cycle gas turbines |
US5320483A (en) * | 1992-12-30 | 1994-06-14 | General Electric Company | Steam and air cooling for stator stage of a turbine |
US5634766A (en) * | 1994-08-23 | 1997-06-03 | General Electric Co. | Turbine stator vane segments having combined air and steam cooling circuits |
US5603606A (en) * | 1994-11-14 | 1997-02-18 | Solar Turbines Incorporated | Turbine cooling system |
JP3781832B2 (ja) * | 1996-08-29 | 2006-05-31 | 株式会社東芝 | ガスタービン |
JP4170400B2 (ja) * | 1997-04-07 | 2008-10-22 | シーメンス アクチエンゲゼルシヤフト | タービン翼、その用途ならびにタービン翼の冷却方法 |
-
1997
- 1997-09-01 DE DE19738065A patent/DE19738065A1/de not_active Ceased
-
1998
- 1998-08-11 DE DE59810315T patent/DE59810315D1/de not_active Expired - Lifetime
- 1998-08-11 EP EP98810770A patent/EP0899425B1/de not_active Expired - Lifetime
- 1998-08-28 US US09/141,586 patent/US6033181A/en not_active Expired - Lifetime
- 1998-08-28 CN CN98116951A patent/CN1120287C/zh not_active Expired - Fee Related
- 1998-08-31 JP JP10245038A patent/JPH11132003A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
EP0899425A3 (de) | 2000-07-05 |
CN1120287C (zh) | 2003-09-03 |
JPH11132003A (ja) | 1999-05-18 |
CN1211667A (zh) | 1999-03-24 |
US6033181A (en) | 2000-03-07 |
DE19738065A1 (de) | 1999-03-04 |
EP0899425A2 (de) | 1999-03-03 |
EP0899425B1 (de) | 2003-12-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8327 | Change in the person/name/address of the patent owner |
Owner name: ALSTOM TECHNOLOGY LTD, BADEN, CH |
|
8328 | Change in the person/name/address of the agent |
Representative=s name: ROESLER, U., DIPL.-PHYS.UNIV., PAT.-ANW., 81241 MUENCHEN |
|
8364 | No opposition during term of opposition |