CH702551B8 - Schaufelblatt mit mehreren Wirbelgeneratoren in inneren Kühlhohlräumen. - Google Patents
Schaufelblatt mit mehreren Wirbelgeneratoren in inneren Kühlhohlräumen. Download PDFInfo
- Publication number
- CH702551B8 CH702551B8 CH00004/11A CH42011A CH702551B8 CH 702551 B8 CH702551 B8 CH 702551B8 CH 00004/11 A CH00004/11 A CH 00004/11A CH 42011 A CH42011 A CH 42011A CH 702551 B8 CH702551 B8 CH 702551B8
- Authority
- CH
- Switzerland
- Prior art keywords
- airfoil
- vortex generators
- trailing edge
- internal cooling
- cooling cavities
- Prior art date
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
-
- 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
- F01D5/186—Film cooling
-
- 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
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
-
- 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
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/127—Vortex generators, turbulators, or the like, for mixing
-
- 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
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2212—Improvement of heat transfer by creating turbulence
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Ein Schaufelblatt (10) enthält eine Vorderkante (12), eine Hinterkante (14), eine Saugseite (16) und eine Druckseite (18), wobei sich mehrere innere Hohlräume (20, 22, 24) innerhalb des Schaufelblattes (10) in Radialrichtung erstrecken, wobei sich ein erster innerer Hohlraum (24) entlang der Hinterkante (14) erstreckt. Die Hinterkante (14) ist mit mehreren entlang dieser angeordneten Kühlmittelaustrittsöffnungen versehen. Mehrere Wirbelgeneratoren sind auf einer Innenfläche der Druckseite (18) und/oder der Saugseite (16) des Schaufelblattes (10) ausgebildet. Die Wirbelgeneratoren sind erfindungsgemäss in einer radial voneinander beabstandeten Anordnung im hinteren inneren Hohlraum (24) angeordnet und erstrecken sich im Wesentlichen parallel zu der Hinterkante (14).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP12405004.8A EP2500458B1 (de) | 2011-01-03 | 2012-01-09 | Aktivierungsvorrichtung zur weg-und zeitabhängigen Bewegung einer Fadenschneid- und Anstickeinheit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/683,133 US8439628B2 (en) | 2010-01-06 | 2010-01-06 | Heat transfer enhancement in internal cavities of turbine engine airfoils |
Publications (3)
Publication Number | Publication Date |
---|---|
CH702551A2 CH702551A2 (de) | 2011-07-15 |
CH702551B1 CH702551B1 (de) | 2015-09-15 |
CH702551B8 true CH702551B8 (de) | 2015-11-30 |
Family
ID=44215088
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH00004/11A CH702551B8 (de) | 2010-01-06 | 2011-01-03 | Schaufelblatt mit mehreren Wirbelgeneratoren in inneren Kühlhohlräumen. |
Country Status (5)
Country | Link |
---|---|
US (1) | US8439628B2 (de) |
JP (1) | JP5898841B2 (de) |
CN (1) | CN102116177B (de) |
CH (1) | CH702551B8 (de) |
DE (1) | DE102010061376A1 (de) |
Families Citing this family (27)
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US8757701B2 (en) * | 2010-01-15 | 2014-06-24 | Aeroserve Technologies, Ltd. | Drag reduction device for transport vehicles having randomized irregular shaped edge vortex generating channels |
US9249675B2 (en) | 2011-08-30 | 2016-02-02 | General Electric Company | Pin-fin array |
US9506351B2 (en) | 2012-04-27 | 2016-11-29 | General Electric Company | Durable turbine vane |
US9995148B2 (en) | 2012-10-04 | 2018-06-12 | General Electric Company | Method and apparatus for cooling gas turbine and rotor blades |
US9850762B2 (en) | 2013-03-13 | 2017-12-26 | General Electric Company | Dust mitigation for turbine blade tip turns |
US20150003962A1 (en) * | 2013-06-27 | 2015-01-01 | Bruce L. Smith | Apparatus for reducing a temperature gradient of mainstream fluid downstream of an airfoil in a gas turbine engine |
JP6245740B2 (ja) * | 2013-11-20 | 2017-12-13 | 三菱日立パワーシステムズ株式会社 | ガスタービン翼 |
EP2886797B1 (de) * | 2013-12-20 | 2018-11-28 | Ansaldo Energia Switzerland AG | Ein hohle gekühlte Rotor- oder Leitschaufel einer Gasturbine, wobei die kühlkanäle Stifte mit Verbindungsstreben beinhalten |
WO2015094531A1 (en) | 2013-12-20 | 2015-06-25 | United Technologies Corporation | Gas turbine engine component cooling cavity with vortex promoting features |
WO2015154729A1 (en) * | 2014-04-07 | 2015-10-15 | Prihoda S.R.O. | Air-conditioning element for air distribution |
US9476406B2 (en) * | 2014-04-14 | 2016-10-25 | Siemens Aktiengesellschaft | Vortex generators aligned with trailing edge features on wind turbine blade |
US9957816B2 (en) | 2014-05-29 | 2018-05-01 | General Electric Company | Angled impingement insert |
EP3149279A1 (de) | 2014-05-29 | 2017-04-05 | General Electric Company | Fastback-turbulator |
US10364684B2 (en) | 2014-05-29 | 2019-07-30 | General Electric Company | Fastback vorticor pin |
US10422235B2 (en) | 2014-05-29 | 2019-09-24 | General Electric Company | Angled impingement inserts with cooling features |
EP3149284A2 (de) | 2014-05-29 | 2017-04-05 | General Electric Company | Motorkomponenten mit prallkühlungsfunktionen |
US10233775B2 (en) | 2014-10-31 | 2019-03-19 | General Electric Company | Engine component for a gas turbine engine |
US10280785B2 (en) | 2014-10-31 | 2019-05-07 | General Electric Company | Shroud assembly for a turbine engine |
US9777635B2 (en) * | 2014-12-31 | 2017-10-03 | General Electric Company | Engine component |
EP3436669B1 (de) * | 2016-03-31 | 2023-06-07 | Siemens Energy Global GmbH & Co. KG | Turbinenschaufel mit internen kühlkanälen mit strömungsteilung |
US10655477B2 (en) * | 2016-07-26 | 2020-05-19 | General Electric Company | Turbine components and method for forming turbine components |
WO2018186891A1 (en) * | 2017-04-07 | 2018-10-11 | General Electric Company | Cooling assembly for a turbine assembly |
US10494948B2 (en) * | 2017-05-09 | 2019-12-03 | General Electric Company | Impingement insert |
CN106988790A (zh) * | 2017-06-08 | 2017-07-28 | 哈尔滨工业大学 | 一种高温涡轮动叶顶部对转涡的冷却结构 |
US10458253B2 (en) | 2018-01-08 | 2019-10-29 | United Technologies Corporation | Gas turbine engine components having internal hybrid cooling cavities |
CN108910019B (zh) * | 2018-07-05 | 2020-03-31 | 中国空气动力研究与发展中心高速空气动力研究所 | 一种采用热双金属微锯齿结构的空气流动控制系统 |
CN114763748A (zh) * | 2021-01-12 | 2022-07-19 | 上海交通大学 | 带有表面微型涡发生器的气膜冷却结构 |
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-
2010
- 2010-01-06 US US12/683,133 patent/US8439628B2/en active Active
- 2010-12-20 DE DE102010061376A patent/DE102010061376A1/de active Pending
- 2010-12-27 JP JP2010289321A patent/JP5898841B2/ja active Active
-
2011
- 2011-01-03 CH CH00004/11A patent/CH702551B8/de not_active IP Right Cessation
- 2011-01-05 CN CN201110000959.1A patent/CN102116177B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
CH702551A2 (de) | 2011-07-15 |
CN102116177B (zh) | 2015-05-20 |
US8439628B2 (en) | 2013-05-14 |
CH702551B1 (de) | 2015-09-15 |
JP5898841B2 (ja) | 2016-04-06 |
CN102116177A (zh) | 2011-07-06 |
JP2011140951A (ja) | 2011-07-21 |
US20110164960A1 (en) | 2011-07-07 |
DE102010061376A1 (de) | 2011-07-07 |
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PK | Correction |
Free format text: ERFINDER BERICHTIGT. |
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Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH |
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PL | Patent ceased |