CH706962A8 - Serpentinenkühlung der Leitschaufelendwand. - Google Patents

Serpentinenkühlung der Leitschaufelendwand.

Info

Publication number
CH706962A8
CH706962A8 CH01511/13A CH15112013A CH706962A8 CH 706962 A8 CH706962 A8 CH 706962A8 CH 01511/13 A CH01511/13 A CH 01511/13A CH 15112013 A CH15112013 A CH 15112013A CH 706962 A8 CH706962 A8 CH 706962A8
Authority
CH
Switzerland
Prior art keywords
end wall
vane end
serpentine cooling
leading edge
inlet
Prior art date
Application number
CH01511/13A
Other languages
English (en)
Other versions
CH706962B1 (de
CH706962A2 (de
Inventor
Daniel Jackson Dillard
Christopher Donald Porter
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH706962A2 publication Critical patent/CH706962A2/de
Publication of CH706962A8 publication Critical patent/CH706962A8/de
Publication of CH706962B1 publication Critical patent/CH706962B1/de

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
    • 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
    • F05D2240/81—Cooled platforms
    • 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
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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
    • F05D2260/204—Heat transfer, e.g. cooling by the use of microcircuits
    • 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

Abstract

Ein Gasturbinenleitschaufelabschnitt (100) einer Gasturbine weist eine innere Endwand (114) mit einer Vorderkante (115) auf. Ein Serpentinenkanal (116) ist im Wesentlichen innerhalb der Vorderkante (115) eingerichtet. Der Serpentinenkanal (116) weist einen Einlass und einen Auslass auf. Luft kann an dem Einlass (118) aufgenommen und unter Kühlung der Vorderkante (117) an dem Auslass (119) ausgegeben werden.
CH01511/13A 2012-09-10 2013-09-04 Serpentinenkühlung der Leitschaufelendwand. CH706962B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/608,269 US9194237B2 (en) 2012-09-10 2012-09-10 Serpentine cooling of nozzle endwall

Publications (3)

Publication Number Publication Date
CH706962A2 CH706962A2 (de) 2014-03-14
CH706962A8 true CH706962A8 (de) 2014-08-29
CH706962B1 CH706962B1 (de) 2017-12-15

Family

ID=50153443

Family Applications (1)

Application Number Title Priority Date Filing Date
CH01511/13A CH706962B1 (de) 2012-09-10 2013-09-04 Serpentinenkühlung der Leitschaufelendwand.

Country Status (4)

Country Link
US (1) US9194237B2 (de)
JP (1) JP2014051981A (de)
CH (1) CH706962B1 (de)
DE (1) DE102013109150A1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6613803B2 (ja) 2015-10-22 2019-12-04 三菱日立パワーシステムズ株式会社 翼、これを備えているガスタービン、及び翼の製造方法
US10174622B2 (en) 2016-04-12 2019-01-08 Solar Turbines Incorporated Wrapped serpentine passages for turbine blade cooling
US20180230815A1 (en) * 2017-02-15 2018-08-16 Florida Turbine Technologies, Inc. Turbine airfoil with thin trailing edge cooling circuit
US10890074B2 (en) * 2018-05-01 2021-01-12 Raytheon Technologies Corporation Coriolis optimized u-channel with platform core
US11174788B1 (en) * 2020-05-15 2021-11-16 General Electric Company Systems and methods for cooling an endwall in a rotary machine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3844679A (en) * 1973-03-28 1974-10-29 Gen Electric Pressurized serpentine cooling channel construction for open-circuit liquid cooled turbine buckets
US4353679A (en) * 1976-07-29 1982-10-12 General Electric Company Fluid-cooled element
JPH0552102A (ja) * 1991-08-23 1993-03-02 Toshiba Corp ガスタービン
EP0791127B1 (de) 1994-11-10 2000-03-08 Siemens Westinghouse Power Corporation Gasturbinenschaufel mit einer gekühlten plattform
JP2971386B2 (ja) * 1996-01-08 1999-11-02 三菱重工業株式会社 ガスタービン静翼
JP3495579B2 (ja) 1997-10-28 2004-02-09 三菱重工業株式会社 ガスタービン静翼
US6065928A (en) * 1998-07-22 2000-05-23 General Electric Company Turbine nozzle having purge air circuit
US6254333B1 (en) 1999-08-02 2001-07-03 United Technologies Corporation Method for forming a cooling passage and for cooling a turbine section of a rotary machine
US7416391B2 (en) * 2006-02-24 2008-08-26 General Electric Company Bucket platform cooling circuit and method
WO2008081486A1 (en) * 2007-01-04 2008-07-10 Ansaldo Energia S.P.A. Spacer for gas turbine blade insert
US8061979B1 (en) * 2007-10-19 2011-11-22 Florida Turbine Technologies, Inc. Turbine BOAS with edge cooling
JP5078766B2 (ja) * 2008-06-13 2012-11-21 三菱重工業株式会社 タービン静翼構造
US8167558B2 (en) * 2009-01-19 2012-05-01 Siemens Energy, Inc. Modular serpentine cooling systems for turbine engine components
US8096772B2 (en) * 2009-03-20 2012-01-17 Siemens Energy, Inc. Turbine vane for a gas turbine engine having serpentine cooling channels within the inner endwall
US8221055B1 (en) * 2009-07-08 2012-07-17 Florida Turbine Technologies, Inc. Turbine stator vane with endwall cooling

Also Published As

Publication number Publication date
US20140072400A1 (en) 2014-03-13
DE102013109150A1 (de) 2014-03-13
US9194237B2 (en) 2015-11-24
CH706962B1 (de) 2017-12-15
CH706962A2 (de) 2014-03-14
JP2014051981A (ja) 2014-03-20

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Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH