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DE60112551D1 - Schaufel für eine axial durchströmte turbomaschine - Google Patents

Schaufel für eine axial durchströmte turbomaschine

Info

Publication number
DE60112551D1
DE60112551D1 DE60112551T DE60112551T DE60112551D1 DE 60112551 D1 DE60112551 D1 DE 60112551D1 DE 60112551 T DE60112551 T DE 60112551T DE 60112551 T DE60112551 T DE 60112551T DE 60112551 D1 DE60112551 D1 DE 60112551D1
Authority
DE
Germany
Prior art keywords
aerofoil
platform
turbine
vane
sections
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE60112551T
Other languages
English (en)
Other versions
DE60112551T2 (de
Inventor
Robert Haller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens AG
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 DE60112551D1 publication Critical patent/DE60112551D1/de
Publication of DE60112551T2 publication Critical patent/DE60112551T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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)
DE60112551T 2000-02-17 2001-02-19 Schaufel für eine axial durchströmte turbomaschine Expired - Lifetime DE60112551T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GBGB0003676.4A GB0003676D0 (en) 2000-02-17 2000-02-17 Aerofoils
GB0003676 2000-02-17
PCT/GB2001/000682 WO2001061152A1 (en) 2000-02-17 2001-02-19 Aerofoil for an axial flow turbomachine

Publications (2)

Publication Number Publication Date
DE60112551D1 true DE60112551D1 (de) 2005-09-15
DE60112551T2 DE60112551T2 (de) 2006-06-08

Family

ID=9885797

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60112551T Expired - Lifetime DE60112551T2 (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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EP2133573B1 (de) 2008-06-13 2011-08-17 Siemens Aktiengesellschaft Schaufel für einen Axialflusskompressor
US8147207B2 (en) * 2008-09-04 2012-04-03 Siemens Energy, Inc. Compressor blade having a ratio of leading edge sweep to leading edge dihedral in a range of 1:1 to 3:1 along the radially outer portion
DE102008060847B4 (de) * 2008-12-06 2020-03-19 MTU Aero Engines AG Strömungsmaschine
US8075259B2 (en) * 2009-02-13 2011-12-13 United Technologies Corporation Turbine vane airfoil with turning flow and axial/circumferential trailing edge configuration
US8360731B2 (en) * 2009-12-04 2013-01-29 United Technologies Corporation Tip vortex control
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
US8105044B2 (en) * 2010-04-23 2012-01-31 Pratt & Whitney Canada Corp. Compressor turbine blade airfoil profile
US10287987B2 (en) * 2010-07-19 2019-05-14 United Technologies Corporation Noise reducing vane
ITMI20101447A1 (it) * 2010-07-30 2012-01-30 Alstom Technology Ltd "turbina a vapore a bassa pressione e metodo per il funzionamento della stessa"
US8651806B2 (en) * 2010-08-17 2014-02-18 Hamilton Sundstrand Corporation Air turbine starter inlet housing assembly airflow path
US8672620B2 (en) * 2010-08-17 2014-03-18 Hamilton Sundstrand Corporation Air turbine starter turbine nozzle airfoil
EP2476862B1 (de) * 2011-01-13 2013-11-20 Alstom Technology Ltd Leitschaufel für eine axiale Strömungsmaschine und zugehörige Strömungsmaschine
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
US9255480B2 (en) * 2011-10-28 2016-02-09 General Electric Company Turbine of a turbomachine
US9051843B2 (en) 2011-10-28 2015-06-09 General Electric Company Turbomachine blade including a squeeler pocket
US8992179B2 (en) 2011-10-28 2015-03-31 General Electric Company Turbine of a turbomachine
US9429069B2 (en) * 2012-01-10 2016-08-30 Starrotor Corporation Open brayton bottoming cycle and method of using the same
US8979487B2 (en) * 2012-04-11 2015-03-17 Pratt & Whitney Canada Corp. High pressure turbine vane airfoil profile
GB201217482D0 (en) * 2012-10-01 2012-11-14 Rolls Royce Plc Aerofoil for axial-flow machine
US10495106B2 (en) 2014-02-19 2019-12-03 United Technologies Corporation Gas turbine engine airfoil
ES2717801T3 (es) 2015-10-26 2019-06-25 MTU Aero Engines AG Alabe móvil
GB2544735B (en) * 2015-11-23 2018-02-07 Rolls Royce Plc Vanes of a gas turbine engine
US20170342839A1 (en) * 2016-05-25 2017-11-30 General Electric Company System for a low swirl low pressure 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
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
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
EP3816397B1 (de) * 2019-10-31 2023-05-10 General Electric Company Turbinenschaufel mit kontrollierter strömung
US11566530B2 (en) 2019-11-26 2023-01-31 General Electric Company Turbomachine nozzle with an airfoil having a circular trailing edge
US11629599B2 (en) 2019-11-26 2023-04-18 General Electric Company Turbomachine nozzle with an airfoil having a curvilinear trailing edge
BE1028108B1 (fr) * 2020-02-28 2021-09-28 Safran Aero Boosters Compresseur transsonique de turbomachine
CN113252351B (zh) * 2021-06-10 2021-10-01 中国航发上海商用航空发动机制造有限责任公司 一种缩尺试验件及对外涵分墙导叶的截断方法
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
GB0104002D0 (en) 2001-04-04
ES2243448T3 (es) 2005-12-01
DE60112551T2 (de) 2006-06-08
AU2001233889A1 (en) 2001-08-27
GB2359341A (en) 2001-08-22
EP1259711B1 (de) 2005-08-10
WO2001061152A1 (en) 2001-08-23
EP1259711A1 (de) 2002-11-27
US20020197156A1 (en) 2002-12-26
GB0003676D0 (en) 2000-04-05
US6709233B2 (en) 2004-03-23
JP2003522890A (ja) 2003-07-29
ATE301767T1 (de) 2005-08-15

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition