ATE467749T1 - Gegossene turbinenleitschaufel mit hakensockel - Google Patents

Gegossene turbinenleitschaufel mit hakensockel

Info

Publication number
ATE467749T1
ATE467749T1 AT02001265T AT02001265T ATE467749T1 AT E467749 T1 ATE467749 T1 AT E467749T1 AT 02001265 T AT02001265 T AT 02001265T AT 02001265 T AT02001265 T AT 02001265T AT E467749 T1 ATE467749 T1 AT E467749T1
Authority
AT
Austria
Prior art keywords
blade
platform
outer edge
hook base
base
Prior art date
Application number
AT02001265T
Other languages
English (en)
Inventor
Peter Tiemann
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
Application granted granted Critical
Publication of ATE467749T1 publication Critical patent/ATE467749T1/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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/22—Moulds for peculiarly-shaped castings
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/915—Pump or portion thereof by casting or molding
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
AT02001265T 2002-01-17 2002-01-17 Gegossene turbinenleitschaufel mit hakensockel ATE467749T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP02001265A EP1331361B1 (de) 2002-01-17 2002-01-17 Gegossene Turbinenleitschaufel mit Hakensockel

Publications (1)

Publication Number Publication Date
ATE467749T1 true ATE467749T1 (de) 2010-05-15

Family

ID=8185294

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02001265T ATE467749T1 (de) 2002-01-17 2002-01-17 Gegossene turbinenleitschaufel mit hakensockel

Country Status (6)

Country Link
US (1) US6923620B2 (de)
EP (1) EP1331361B1 (de)
JP (1) JP4303480B2 (de)
CN (1) CN100447374C (de)
AT (1) ATE467749T1 (de)
DE (1) DE50214427D1 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE467889T1 (de) 2003-08-14 2010-05-15 Lg Electronics Inc Aufzeichnungsmedium, konfigurationsverfahren für diesbezügliche steuerinformation, aufzeichnungs- und wiedergabeverfahren sowie gerät dafür
EP1591625A1 (de) * 2004-04-30 2005-11-02 ALSTOM Technology Ltd Deckband für eine Gasturbinenschaufel
US7819629B2 (en) * 2007-02-15 2010-10-26 Siemens Energy, Inc. Blade for a gas turbine
US8356975B2 (en) * 2010-03-23 2013-01-22 United Technologies Corporation Gas turbine engine with non-axisymmetric surface contoured vane platform
US9976433B2 (en) 2010-04-02 2018-05-22 United Technologies Corporation Gas turbine engine with non-axisymmetric surface contoured rotor blade platform
US8739404B2 (en) 2010-11-23 2014-06-03 General Electric Company Turbine components with cooling features and methods of manufacturing the same
EP3147452B1 (de) * 2015-09-22 2018-07-25 Ansaldo Energia IP UK Limited Turbomotor-beschaufelungselement
CN107755637A (zh) * 2017-09-18 2018-03-06 东方电气集团东方汽轮机有限公司 一种消除定向凝固铸件缺陷的方法
US10544699B2 (en) * 2017-12-19 2020-01-28 Rolls-Royce Corporation System and method for minimizing the turbine blade to vane platform overlap gap
CN113560544B (zh) * 2021-06-28 2022-10-25 深圳市万泽中南研究院有限公司 一种定向叶片及其柱状晶组织优化方法
CN115055645B (zh) * 2022-06-07 2023-10-17 中国航发航空科技股份有限公司 导向器叶片毛坯的浇注系统
CN118917015B (zh) * 2024-08-20 2025-04-25 中国船舶集团有限公司第七〇三研究所 涡轮导叶缘板双排圆形微细管阵冷却结构设计方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR965713A (de) 1947-05-07 1950-09-20
US3494709A (en) * 1965-05-27 1970-02-10 United Aircraft Corp Single crystal metallic part
US4902198A (en) 1988-08-31 1990-02-20 Westinghouse Electric Corp. Apparatus for film cooling of turbine van shrouds
US5281097A (en) * 1992-11-20 1994-01-25 General Electric Company Thermal control damper for turbine rotors
US5344283A (en) * 1993-01-21 1994-09-06 United Technologies Corporation Turbine vane having dedicated inner platform cooling
ES2118638T3 (es) * 1994-10-31 1998-09-16 Westinghouse Electric Corp Alabe rotativo de turbina de gas con plataforma refrigerada.
CA2262064C (en) * 1998-02-23 2002-09-03 Mitsubishi Heavy Industries, Ltd. Gas turbine moving blade platform
DE59907300D1 (de) * 1998-04-21 2003-11-13 Siemens Ag Turbinenschaufel
DE10004714C2 (de) * 2000-02-03 2002-03-14 Karl Walter Formen Fa Vorrichtung zum Gießen eines Formteils
EP1145784A1 (de) * 2000-04-12 2001-10-17 Siemens Aktiengesellschaft Gussvorrichtung, insbesondere zur Herstellung von Turbinenschaufeln
DE10024278A1 (de) * 2000-05-17 2001-11-22 Weidmueller Interface Kunststoffgehäuse mit einer Aufnahme sowie Verfahren zu dessen Herstellung
US6454526B1 (en) * 2000-09-28 2002-09-24 Siemens Westinghouse Power Corporation Cooled turbine vane with endcaps
DE10060141A1 (de) * 2000-12-04 2002-06-06 Alstom Switzerland Ltd Verfahren zur Herstellung eines Gussteils, Modellform und keramischer Einsatz zum Gebrauch in diesem Verfahren

Also Published As

Publication number Publication date
US20050111963A1 (en) 2005-05-26
EP1331361B1 (de) 2010-05-12
JP4303480B2 (ja) 2009-07-29
CN1451846A (zh) 2003-10-29
US6923620B2 (en) 2005-08-02
DE50214427D1 (de) 2010-06-24
CN100447374C (zh) 2008-12-31
EP1331361A1 (de) 2003-07-30
JP2003232205A (ja) 2003-08-22

Similar Documents

Publication Publication Date Title
ATE467749T1 (de) Gegossene turbinenleitschaufel mit hakensockel
ATE423643T1 (de) Refraktärmetallkern
DE69206556D1 (de) Schaufeleinsatz für die Luftkühlung von Gasturbinenschaufeln.
DE60037924D1 (de) Strömungsmaschinenschaufel mit innerer Kühlung
DE69507782D1 (de) Luftauslass-Schlitze für die Hinterkante einer Turbinenschaufel mit Filmkühlung
EP1422383A3 (de) Kühlung einer Gasturbinenschaufel
CA2383961A1 (en) Cast airfoil structure with openings which do not require plugging
DE69507451D1 (de) Turbinenschaufelkühlung
FR2858352B1 (fr) Circuit de refroidissement pour aube de turbine
ATE240200T1 (de) Gekühlter spritzgiesshohlraumeinsatz
ATE520487T1 (de) Verfahren zur herstellung von turbinenschaufeln durch schleudergiessen
DE69828757D1 (de) Kühlung der Anströmkante einer Gasturbinenschaufel
EP0911486A3 (de) Kühlung einer Gasturbinenleitschaufel
BRPI0407599B8 (pt) nacela de motor de turbina a gás
AU2003267612A1 (en) Turbine blade turbulator cooling design
CA2281965A1 (fr) Aube de turbine refroidie a bord de fuite amenage
ATE226876T1 (de) Wandsäge und sägeblatt
DE60033768D1 (de) Kern zur Einstellung der Wanddicke einer Turbinenschaufel und Verfahren
BR0303097A (pt) Coquilha refrigerada por lìquido
ATE392800T1 (de) Gehäuse und feldgerät
FR2737838B1 (fr) Systeme de refroidissement integre pour convertisseur de puissance utilisant l'air d'admission d'une turbine
RU2003101665A (ru) Подвижная лопатка турбины высокого давления, снабженная выходной кромкой с улучшенной тепловой характеристикой
DE60310539D1 (de) Abgaskrümmer
AU2001290458A1 (en) A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component
ATE98747T1 (de) Spinnpumpe.

Legal Events

Date Code Title Description
REN Ceased due to non-payment of the annual fee