EP1760321A3 - Schaufel einer Strömungsarbeitsmaschine - Google Patents

Schaufel einer Strömungsarbeitsmaschine Download PDF

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Publication number
EP1760321A3
EP1760321A3 EP06016439A EP06016439A EP1760321A3 EP 1760321 A3 EP1760321 A3 EP 1760321A3 EP 06016439 A EP06016439 A EP 06016439A EP 06016439 A EP06016439 A EP 06016439A EP 1760321 A3 EP1760321 A3 EP 1760321A3
Authority
EP
European Patent Office
Prior art keywords
blade
profile skeleton
angle
line
skeleton line
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.)
Ceased
Application number
EP06016439A
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English (en)
French (fr)
Other versions
EP1760321A2 (de
Inventor
Volker Gümmer
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.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
Rolls Royce Deutschland Ltd and Co KG
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 Rolls Royce Deutschland Ltd and Co KG filed Critical Rolls Royce Deutschland Ltd and Co KG
Publication of EP1760321A2 publication Critical patent/EP1760321A2/de
Publication of EP1760321A3 publication Critical patent/EP1760321A3/de
Ceased legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324Blades
    • 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
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • 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
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/145Means for influencing boundary layers or secondary circulations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • F04D29/544Blade shapes
    • 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
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/301Cross-sectional characteristics
    • 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
    • F05D2250/70Shape
    • F05D2250/71Shape curved
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/02Formulas of curves

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Die Erfindung bezieht sich auf eine Strömungsarbeitsmaschinenschaufel mit einer Profilskelettlinie, welche sich längs einer Meridianstromlinie erstreckt, wobei die Schaufel in radialer Richtung in mindestens drei Zonen (Z0, Z1, Z2) unterteilt ist und wobei die jeweils radial innere und die radial äußere Profilskelettlinie jeder Zone (Z0, Z1, Z2) so ausgebildet ist, dass diese folgenden Gleichungen genügen: α = α 1 α P α 1 α 2
Figure imga0001
S = s P S
Figure imga0002

wobei
- P ein beliebiger Punkt der Profilskelettlinie,
- α1 der Neigungswinkel an der Schaufel-Vorderkante,
- α2 der Neigungswinkel an der Schaufel-Hinterkante,
- α* der dimensionslose, bezogene Winkel der Gesamtwölbung,
- S* die dimensionslose, bezogene Lauflänge,
- αP der Winkel der Tangente an einem beliebigen Punkt P der Profilskelettlinie zur mittleren Meridianstromlinie,
- SP die Lauflänge der Profilskelettlinie an einem beliebigen Punkt P, und
- S die Gesamtlauflänge der Profilskelettlinie sind.
EP06016439A 2005-09-05 2006-08-07 Schaufel einer Strömungsarbeitsmaschine Ceased EP1760321A3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005042115A DE102005042115A1 (de) 2005-09-05 2005-09-05 Schaufel einer Strömungsarbeitsmaschine mit blockweise definierter Profilskelettlinie

Publications (2)

Publication Number Publication Date
EP1760321A2 EP1760321A2 (de) 2007-03-07
EP1760321A3 true EP1760321A3 (de) 2011-07-27

Family

ID=37467618

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06016439A Ceased EP1760321A3 (de) 2005-09-05 2006-08-07 Schaufel einer Strömungsarbeitsmaschine

Country Status (3)

Country Link
US (1) US7419353B2 (de)
EP (1) EP1760321A3 (de)
DE (1) DE102005042115A1 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006055869A1 (de) * 2006-11-23 2008-05-29 Rolls-Royce Deutschland Ltd & Co Kg Schaufelblattdesign für die Lauf- und Leitschaufeln einer Turbomaschine
DE102009033593A1 (de) * 2009-07-17 2011-01-20 Rolls-Royce Deutschland Ltd & Co Kg Triebwerkschaufel mit überhöhter Vorderkantenbelastung
DE102010009615B4 (de) 2010-02-27 2016-11-17 MTU Aero Engines AG Schaufelblatt mit gefädelten Profilschnitten
DE102010027588A1 (de) * 2010-07-19 2012-01-19 Rolls-Royce Deutschland Ltd & Co Kg Fan-Nachleitradschaufel eines Turbofantriebwerks
JP5608062B2 (ja) * 2010-12-10 2014-10-15 株式会社日立製作所 遠心型ターボ機械
US9309769B2 (en) * 2010-12-28 2016-04-12 Rolls-Royce Corporation Gas turbine engine airfoil shaped component
FR2991373B1 (fr) * 2012-05-31 2014-06-20 Snecma Aube de soufflante pour turboreacteur d'avion a profil cambre en sections de pied
JP6468414B2 (ja) * 2014-08-12 2019-02-13 株式会社Ihi 圧縮機静翼、軸流圧縮機、及びガスタービン
EP3051142B1 (de) 2015-01-28 2017-10-11 MTU Aero Engines GmbH Gasturbinen-axialverdichter
US10577973B2 (en) 2016-02-18 2020-03-03 General Electric Company Service tube for a turbine engine
DE102016115868A1 (de) * 2016-08-26 2018-03-01 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit hohem Ausnutzungsgrad
GB201719538D0 (en) 2017-11-24 2018-01-10 Rolls Royce Plc Gas turbine engine
GB201719539D0 (en) * 2017-11-24 2018-01-10 Rolls Royce Plc Gas Turbine Engine
JP6774044B2 (ja) 2017-12-20 2020-10-21 株式会社Ihi ファン及び圧縮機の静翼
IT202000005146A1 (it) * 2020-03-11 2021-09-11 Ge Avio Srl Motore a turbina con profilo aerodinamico avente alta accelerazione e bassa curva di paletta
US11286779B2 (en) * 2020-06-03 2022-03-29 Honeywell International Inc. Characteristic distribution for rotor blade of booster rotor

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2660401A (en) * 1951-08-07 1953-11-24 Gen Electric Turbine bucket
US2663493A (en) * 1949-04-26 1953-12-22 A V Roe Canada Ltd Blading for compressors, turbines, and the like
GB719061A (en) * 1950-06-21 1954-11-24 United Aircraft Corp Blade arrangement for improving the performance of a gas turbine plant
EP0833060A2 (de) * 1996-09-30 1998-04-01 Kabushiki Kaisha Toshiba Schaufel für axiale Strömungsmaschine
FR2828709A1 (fr) * 2001-08-17 2003-02-21 Snecma Moteurs Aube de redresseur
EP1452741A1 (de) * 2003-02-27 2004-09-01 Snecma Moteurs Gekrümmte Schaufel für Strahltriebwerk

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4431376A (en) 1980-10-27 1984-02-14 United Technologies Corporation Airfoil shape for arrays of airfoils
JP3082378B2 (ja) 1991-12-20 2000-08-28 株式会社デンソー 送風ファン
DE4344189C1 (de) 1993-12-23 1995-08-03 Mtu Muenchen Gmbh Axial-Schaufelgitter mit gepfeilten Schaufelvorderkanten
JP3816150B2 (ja) * 1995-07-18 2006-08-30 株式会社荏原製作所 遠心流体機械
US6244817B1 (en) * 1996-12-05 2001-06-12 Mcdonnell Douglas Corporation Method and apparatus for a fan noise controller
ES2212251T3 (es) * 1998-03-23 2004-07-16 Spal S.R.L. Ventilador de flujo axial.
EP0945625B1 (de) 1998-03-23 2004-03-03 SPAL S.r.l. Axiallüfter
US6299412B1 (en) 1999-12-06 2001-10-09 General Electric Company Bowed compressor airfoil
US6331100B1 (en) 1999-12-06 2001-12-18 General Electric Company Doubled bowed compressor airfoil

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2663493A (en) * 1949-04-26 1953-12-22 A V Roe Canada Ltd Blading for compressors, turbines, and the like
GB719061A (en) * 1950-06-21 1954-11-24 United Aircraft Corp Blade arrangement for improving the performance of a gas turbine plant
US2660401A (en) * 1951-08-07 1953-11-24 Gen Electric Turbine bucket
EP0833060A2 (de) * 1996-09-30 1998-04-01 Kabushiki Kaisha Toshiba Schaufel für axiale Strömungsmaschine
FR2828709A1 (fr) * 2001-08-17 2003-02-21 Snecma Moteurs Aube de redresseur
EP1452741A1 (de) * 2003-02-27 2004-09-01 Snecma Moteurs Gekrümmte Schaufel für Strahltriebwerk

Also Published As

Publication number Publication date
DE102005042115A1 (de) 2007-03-08
US20070053779A1 (en) 2007-03-08
US7419353B2 (en) 2008-09-02
EP1760321A2 (de) 2007-03-07

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