IN2014DN05979A - - Google Patents
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- Publication number
- IN2014DN05979A IN2014DN05979A IN5979DEN2014A IN2014DN05979A IN 2014DN05979 A IN2014DN05979 A IN 2014DN05979A IN 5979DEN2014 A IN5979DEN2014 A IN 5979DEN2014A IN 2014DN05979 A IN2014DN05979 A IN 2014DN05979A
- Authority
- IN
- India
- Prior art keywords
- guide vane
- turbine guide
- coolant
- throttle element
- channel system
- Prior art date
Links
- 239000002826 coolant Substances 0.000 abstract 4
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
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- 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
-
- 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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/185—Two-dimensional patterned serpentine-like
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The invention relates to a turbine guide vane (10) having an aerodynamically bent vane airfoil (14) which has a channel system (28) equipped with a throttle element (32) said channel system comprising channel sections (26) for the guidance of coolant. In order to provide an alternative turbine guide vane (10) by means of which both a partial coolant flow flowing in the interior and a partial coolant flow guided out of the turbine guide vane (10) are adjustable it is proposed that the throttle element (32) is designed for the removal of coolant.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP12155394.5A EP2628900A1 (en) | 2012-02-14 | 2012-02-14 | Turbine vane with a throttling element |
| PCT/EP2012/075256 WO2013120560A1 (en) | 2012-02-14 | 2012-12-12 | Turbine guide vane with a throttle element |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IN2014DN05979A true IN2014DN05979A (en) | 2015-06-26 |
Family
ID=47469943
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IN5979DEN2014 IN2014DN05979A (en) | 2012-02-14 | 2012-12-12 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US9856738B2 (en) |
| EP (2) | EP2628900A1 (en) |
| JP (1) | JP6005764B2 (en) |
| CN (1) | CN104126054B (en) |
| IN (1) | IN2014DN05979A (en) |
| RU (1) | RU2615091C2 (en) |
| WO (1) | WO2013120560A1 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104481927A (en) * | 2014-12-12 | 2015-04-01 | 常州环能涡轮动力股份有限公司 | Flow guiding ring with double-faced centrifugal pressure wheel for micro turbine jet engine |
| EP3147455A1 (en) | 2015-09-23 | 2017-03-29 | Siemens Aktiengesellschaft | Turbine vane with a throttling arrangement |
| EP3199760A1 (en) * | 2016-01-29 | 2017-08-02 | Siemens Aktiengesellschaft | Turbine blade with a throttle element |
| CN109374275A (en) * | 2018-11-13 | 2019-02-22 | 霍山嘉远智能制造有限公司 | A kind of inner flow passage detecting tool of turborotor |
| KR102207971B1 (en) * | 2019-06-21 | 2021-01-26 | 두산중공업 주식회사 | Vane for turbine, turbine including the same |
| US11512640B2 (en) * | 2020-02-12 | 2022-11-29 | General Electric Company | Gas turbine module ventilation system having a controllable baffle vane |
| CN112539086A (en) * | 2020-10-27 | 2021-03-23 | 哈尔滨广瀚燃气轮机有限公司 | Sectional rotary supercharging device for cooling air of turbine rotor blade |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2468727A1 (en) * | 1979-10-26 | 1981-05-08 | Snecma | IMPROVEMENT TO COOLED TURBINE AUBES |
| US4526551A (en) * | 1980-05-30 | 1985-07-02 | Champion Spark Plug Company | Production of electrodes |
| JPS57153903A (en) * | 1981-03-20 | 1982-09-22 | Hitachi Ltd | Cooling structure for turbing blade |
| US4526512A (en) * | 1983-03-28 | 1985-07-02 | General Electric Co. | Cooling flow control device for turbine blades |
| DE3603350A1 (en) | 1986-02-04 | 1987-08-06 | Walter Prof Dipl Ph Sibbertsen | METHOD FOR COOLING THERMALLY LOADED COMPONENTS OF FLOWING MACHINES, DEVICE FOR CARRYING OUT THE METHOD AND TRAINING THERMALLY LOADED BLADES |
| US4666368A (en) | 1986-05-01 | 1987-05-19 | General Electric Company | Swirl nozzle for a cooling system in gas turbine engines |
| JPH09303103A (en) * | 1996-05-16 | 1997-11-25 | Toshiba Corp | Closed loop cooled turbine blade |
| JPH10306701A (en) * | 1997-05-08 | 1998-11-17 | Toshiba Corp | Turbine rotor blade and method of manufacturing the same |
| RU2159335C1 (en) | 1999-04-28 | 2000-11-20 | Открытое акционерное общество "А.Люлька-Сатурн" | Method of cooling turbine wheel rotor of multimode turbojet engine |
| EP1099825A1 (en) * | 1999-11-12 | 2001-05-16 | Siemens Aktiengesellschaft | Turbine blade and production method therefor |
| US7185662B2 (en) * | 2003-11-14 | 2007-03-06 | United Technologies Corporation | Methods of preparing, cleaning and repairing article and article repaired |
| EP1789654B1 (en) * | 2004-09-16 | 2017-08-23 | General Electric Technology GmbH | Turbine engine vane with fluid cooled shroud |
| US8016547B2 (en) * | 2008-01-22 | 2011-09-13 | United Technologies Corporation | Radial inner diameter metering plate |
| ES2542064T3 (en) * | 2008-03-28 | 2015-07-30 | Alstom Technology Ltd | Guide blade for a gas turbine and gas turbine with a guide blade of this class |
| RU2387846C1 (en) * | 2008-10-29 | 2010-04-27 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") | Method to cool by-pass gas turbine engine vanes and device to this end |
-
2012
- 2012-02-14 EP EP12155394.5A patent/EP2628900A1/en not_active Withdrawn
- 2012-12-12 CN CN201280069754.1A patent/CN104126054B/en active Active
- 2012-12-12 WO PCT/EP2012/075256 patent/WO2013120560A1/en not_active Ceased
- 2012-12-12 US US14/376,428 patent/US9856738B2/en active Active
- 2012-12-12 JP JP2014555956A patent/JP6005764B2/en not_active Expired - Fee Related
- 2012-12-12 RU RU2014136803A patent/RU2615091C2/en active
- 2012-12-12 EP EP12808764.0A patent/EP2788583B1/en active Active
- 2012-12-12 IN IN5979DEN2014 patent/IN2014DN05979A/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| JP6005764B2 (en) | 2016-10-12 |
| US9856738B2 (en) | 2018-01-02 |
| CN104126054A (en) | 2014-10-29 |
| EP2788583B1 (en) | 2016-03-02 |
| JP2015507129A (en) | 2015-03-05 |
| US20140377058A1 (en) | 2014-12-25 |
| EP2788583A1 (en) | 2014-10-15 |
| RU2615091C2 (en) | 2017-04-03 |
| CN104126054B (en) | 2016-02-03 |
| WO2013120560A1 (en) | 2013-08-22 |
| RU2014136803A (en) | 2016-04-10 |
| EP2628900A1 (en) | 2013-08-21 |
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