ATE301767T1 - Schaufel für eine axial durchströmte turbomaschine - Google Patents

Schaufel für eine axial durchströmte turbomaschine

Info

Publication number
ATE301767T1
ATE301767T1 AT01905923T AT01905923T ATE301767T1 AT E301767 T1 ATE301767 T1 AT E301767T1 AT 01905923 T AT01905923 T AT 01905923T AT 01905923 T AT01905923 T AT 01905923T AT E301767 T1 ATE301767 T1 AT E301767T1
Authority
AT
Austria
Prior art keywords
aerofoil
platform
turbine
vane
sections
Prior art date
Application number
AT01905923T
Other languages
English (en)
Inventor
Brian Robert Haller
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 ATE301767T1 publication Critical patent/ATE301767T1/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
    • 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
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • 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
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/02—Formulas of curves
    • 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
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/05—Variable camber or chord length

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)
AT01905923T 2000-02-17 2001-02-19 Schaufel für eine axial durchströmte turbomaschine ATE301767T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0003676.4A GB0003676D0 (en) 2000-02-17 2000-02-17 Aerofoils
PCT/GB2001/000682 WO2001061152A1 (en) 2000-02-17 2001-02-19 Aerofoil for an axial flow turbomachine

Publications (1)

Publication Number Publication Date
ATE301767T1 true ATE301767T1 (de) 2005-08-15

Family

ID=9885797

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01905923T ATE301767T1 (de) 2000-02-17 2001-02-19 Schaufel für eine axial durchströmte turbomaschine

Country Status (9)

Country Link
US (1) US6709233B2 (de)
EP (1) EP1259711B1 (de)
JP (1) JP2003522890A (de)
AT (1) ATE301767T1 (de)
AU (1) AU2001233889A1 (de)
DE (1) DE60112551T2 (de)
ES (1) ES2243448T3 (de)
GB (2) GB0003676D0 (de)
WO (1) WO2001061152A1 (de)

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US8894376B2 (en) * 2011-10-28 2014-11-25 General Electric Company Turbomachine blade with tip flare
US8967959B2 (en) * 2011-10-28 2015-03-03 General Electric Company Turbine of a turbomachine
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US10443392B2 (en) * 2016-07-13 2019-10-15 Safran Aircraft Engines Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine
US10443393B2 (en) * 2016-07-13 2019-10-15 Safran Aircraft Engines Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the seventh stage of a turbine
CN109578085B (zh) * 2018-12-26 2021-06-22 中国船舶重工集团公司第七0三研究所 一种通过导叶倾斜减弱涡轮动叶非定常作用力的方法
JP7029181B2 (ja) * 2019-04-22 2022-03-03 株式会社アテクト ノズルベーン
PL3816397T3 (pl) * 2019-10-31 2023-06-19 General Electric Company Łopatki turbiny o kontrolowanym przepływie
US11629599B2 (en) 2019-11-26 2023-04-18 General Electric Company Turbomachine nozzle with an airfoil having a curvilinear trailing edge
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CN115013089B (zh) * 2022-06-09 2023-03-07 西安交通大学 宽工况后向遮挡的涡轮后机匣整流支板设计方法及系统
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Also Published As

Publication number Publication date
GB0003676D0 (en) 2000-04-05
AU2001233889A1 (en) 2001-08-27
GB2359341A (en) 2001-08-22
DE60112551D1 (de) 2005-09-15
DE60112551T2 (de) 2006-06-08
US6709233B2 (en) 2004-03-23
WO2001061152A1 (en) 2001-08-23
EP1259711A1 (de) 2002-11-27
ES2243448T3 (es) 2005-12-01
GB0104002D0 (en) 2001-04-04
US20020197156A1 (en) 2002-12-26
EP1259711B1 (de) 2005-08-10
JP2003522890A (ja) 2003-07-29

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Legal Events

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