EP0823539A3 - Grenzschichtbeeinflussung bei Turbomaschinenschaufeln - Google Patents

Grenzschichtbeeinflussung bei Turbomaschinenschaufeln Download PDF

Info

Publication number
EP0823539A3
EP0823539A3 EP97112247A EP97112247A EP0823539A3 EP 0823539 A3 EP0823539 A3 EP 0823539A3 EP 97112247 A EP97112247 A EP 97112247A EP 97112247 A EP97112247 A EP 97112247A EP 0823539 A3 EP0823539 A3 EP 0823539A3
Authority
EP
European Patent Office
Prior art keywords
influencing
boundary layer
turbomachinery blades
turbomachinery
blades
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.)
Granted
Application number
EP97112247A
Other languages
English (en)
French (fr)
Other versions
EP0823539B1 (de
EP0823539A2 (de
Inventor
Volker Dr. Schulte
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
BMW Rolls Royce GmbH
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 BMW Rolls Royce GmbH filed Critical BMW Rolls Royce GmbH
Publication of EP0823539A2 publication Critical patent/EP0823539A2/de
Publication of EP0823539A3 publication Critical patent/EP0823539A3/de
Application granted granted Critical
Publication of EP0823539B1 publication Critical patent/EP0823539B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F05D2260/00Function
    • F05D2260/16Fluid modulation at a certain frequency
    • 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
    • Y10S415/00Rotary kinetic fluid motors or pumps
    • Y10S415/904Tool drive turbine, e.g. dental drill

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP97112247A 1996-08-09 1997-07-17 Grenzschichtbeeinflussung bei Turbomaschinenschaufeln Expired - Lifetime EP0823539B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19632207 1996-08-09
DE19632207A DE19632207A1 (de) 1996-08-09 1996-08-09 Verfahren zur Verhinderung der laminaren Grenzschicht-Ablösung an Turbomaschinen-Schaufeln

Publications (3)

Publication Number Publication Date
EP0823539A2 EP0823539A2 (de) 1998-02-11
EP0823539A3 true EP0823539A3 (de) 1999-11-10
EP0823539B1 EP0823539B1 (de) 2002-04-10

Family

ID=7802258

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97112247A Expired - Lifetime EP0823539B1 (de) 1996-08-09 1997-07-17 Grenzschichtbeeinflussung bei Turbomaschinenschaufeln

Country Status (3)

Country Link
US (1) US5876182A (de)
EP (1) EP0823539B1 (de)
DE (2) DE19632207A1 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6027305A (en) * 1997-08-13 2000-02-22 Virginia Tech Intellectual Properties, Inc. Method and apparatus for reducing high-cycle fatigue and suppressing noise in rotating machinery
US6203269B1 (en) 1999-02-25 2001-03-20 United Technologies Corporation Centrifugal air flow control
US6435814B1 (en) * 2000-05-16 2002-08-20 General Electric Company Film cooling air pocket in a closed loop cooled airfoil
DE10355240A1 (de) 2003-11-26 2005-07-07 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Fluidentnahme
DE10355241A1 (de) * 2003-11-26 2005-06-30 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Fluidzufuhr
DE102004030597A1 (de) 2004-06-24 2006-01-26 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Aussenradstrahlerzeugung am Stator
DE102004043036A1 (de) 2004-09-06 2006-03-09 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Fluidentnahme
DE102004055439A1 (de) 2004-11-17 2006-05-24 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit dynamischer Strömungsbeeinflussung
US20080149205A1 (en) * 2006-12-20 2008-06-26 General Electric Company System and method for reducing wake
DE102007037924A1 (de) 2007-08-10 2009-02-12 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Ringkanalwandausnehmung
DE102008011644A1 (de) 2008-02-28 2009-09-03 Rolls-Royce Deutschland Ltd & Co Kg Gehäusestrukturierung für Axialverdichter im Nabenbereich
DE102008031982A1 (de) 2008-07-07 2010-01-14 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Nut an einem Laufspalt eines Schaufelendes
DE102008037154A1 (de) 2008-08-08 2010-02-11 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine
DE102008052409A1 (de) 2008-10-21 2010-04-22 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit saugseitennaher Randenergetisierung
US8556576B2 (en) * 2010-09-30 2013-10-15 Florida Turbine Technologies, Inc. Cooled IBR for a micro-turbine
JP2015048716A (ja) * 2013-08-30 2015-03-16 株式会社東芝 蒸気タービン
US10738619B2 (en) * 2014-01-16 2020-08-11 Raytheon Technologies Corporation Fan cooling hole array
US10731469B2 (en) 2016-05-16 2020-08-04 Raytheon Technologies Corporation Method and apparatus to enhance laminar flow for gas turbine engine components
JP6603971B2 (ja) * 2016-08-09 2019-11-13 三菱重工コンプレッサ株式会社 蒸気タービン
US10247015B2 (en) 2017-01-13 2019-04-02 Rolls-Royce Corporation Cooled blisk with dual wall blades for gas turbine engine
US10415403B2 (en) 2017-01-13 2019-09-17 Rolls-Royce North American Technologies Inc. Cooled blisk for gas turbine engine
US10934865B2 (en) 2017-01-13 2021-03-02 Rolls-Royce Corporation Cooled single walled blisk for gas turbine engine
EP3717784B1 (de) 2017-11-28 2024-03-06 Ohio State Innovation Foundation Fluidischer oszillator mit variabler charakteristik und fluidoszillator mit dreidimensionalem auskoppelstrahl und zugehörige verfahren
US10718218B2 (en) 2018-03-05 2020-07-21 Rolls-Royce North American Technologies Inc. Turbine blisk with airfoil and rim cooling
EP3976975A4 (de) * 2019-05-29 2023-06-21 Ohio State Innovation Foundation Versetzter gekrümmter fluidischer oszillator
IT202100000296A1 (it) 2021-01-08 2022-07-08 Gen Electric Motore a turbine con paletta avente un insieme di fossette

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4581887A (en) * 1984-10-19 1986-04-15 The United States Of America As Represented By The Secretary Of The Army Pulsation valve
DE3505823A1 (de) * 1985-02-20 1986-08-21 Hans 8038 Gröbenzell Bischoff Anordnung zur beeinflussung der stroemung an leit- oder laufschaufeln fuer turbomaschinen
US5029440A (en) * 1990-01-26 1991-07-09 The United States Of America As Represented By The Secretary Of The Air Force Acoustical anti-icing system
US5397217A (en) * 1992-11-24 1995-03-14 General Electric Company Pulse-cooled gas turbine engine assembly

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3043567C2 (de) 1980-11-15 1982-09-23 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln Anordnung zur Beeinflussung der Strömung an aerodynamischen Profilen
DE3738366A1 (de) * 1987-11-12 1989-05-24 Deutsche Forsch Luft Raumfahrt Verfahren und vorrichtung zur erzeugung eines laminar-turbulenten grenzschichtuebergangs bei umstroemten koerpern
DE4333865C1 (de) * 1993-10-05 1995-02-16 Mtu Muenchen Gmbh Schaufelblatt für eine Gasturbine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4581887A (en) * 1984-10-19 1986-04-15 The United States Of America As Represented By The Secretary Of The Army Pulsation valve
DE3505823A1 (de) * 1985-02-20 1986-08-21 Hans 8038 Gröbenzell Bischoff Anordnung zur beeinflussung der stroemung an leit- oder laufschaufeln fuer turbomaschinen
US5029440A (en) * 1990-01-26 1991-07-09 The United States Of America As Represented By The Secretary Of The Air Force Acoustical anti-icing system
US5397217A (en) * 1992-11-24 1995-03-14 General Electric Company Pulse-cooled gas turbine engine assembly

Also Published As

Publication number Publication date
EP0823539B1 (de) 2002-04-10
EP0823539A2 (de) 1998-02-11
US5876182A (en) 1999-03-02
DE59706939D1 (de) 2002-05-16
DE19632207A1 (de) 1998-02-12

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