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
Application number
Inventor
Fathi Ahmad
Nihal Kurt
Mario Nitsche
Marco Schüler
Andreas Varnholt
Original Assignee
Siemens Ag
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Siemens Ag filed Critical Siemens Ag
Publication of IN2014DN05979A publication Critical patent/IN2014DN05979A/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • F01D5/188Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/18Two-dimensional patterned
    • F05D2250/185Two-dimensional patterned serpentine-like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/221Improvement 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.
IN5979DEN2014 2012-02-14 2012-12-12 IN2014DN05979A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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
WO2006029983A1 (en) * 2004-09-16 2006-03-23 Alstom Technology Ltd 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

Also Published As

Publication number Publication date
JP2015507129A (en) 2015-03-05
EP2788583B1 (en) 2016-03-02
US9856738B2 (en) 2018-01-02
WO2013120560A1 (en) 2013-08-22
EP2628900A1 (en) 2013-08-21
CN104126054A (en) 2014-10-29
JP6005764B2 (en) 2016-10-12
RU2014136803A (en) 2016-04-10
CN104126054B (en) 2016-02-03
US20140377058A1 (en) 2014-12-25
EP2788583A1 (en) 2014-10-15
RU2615091C2 (en) 2017-04-03

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