FR2485620B1 - Dispositif pour reduire les pertes secondaires dans un conduit d'ecoulement de turbomachine muni d'aubages - Google Patents

Dispositif pour reduire les pertes secondaires dans un conduit d'ecoulement de turbomachine muni d'aubages

Info

Publication number
FR2485620B1
FR2485620B1 FR8111803A FR8111803A FR2485620B1 FR 2485620 B1 FR2485620 B1 FR 2485620B1 FR 8111803 A FR8111803 A FR 8111803A FR 8111803 A FR8111803 A FR 8111803A FR 2485620 B1 FR2485620 B1 FR 2485620B1
Authority
FR
France
Prior art keywords
blades
flow duct
reducing secondary
secondary losses
turbomachine flow
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
Application number
FR8111803A
Other languages
English (en)
Other versions
FR2485620A1 (fr
Inventor
Hans Bischoff
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen 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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2485620A1 publication Critical patent/FR2485620A1/fr
Application granted granted Critical
Publication of FR2485620B1 publication Critical patent/FR2485620B1/fr
Expired 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
    • 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
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • 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
    • Y10S415/914—Device to control boundary layer

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)
FR8111803A 1980-06-24 1981-06-16 Dispositif pour reduire les pertes secondaires dans un conduit d'ecoulement de turbomachine muni d'aubages Expired FR2485620B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3023466A DE3023466C2 (de) 1980-06-24 1980-06-24 Einrichtung zur Verminderung von Sekundärströmungsverlusten in einem beschaufelten Strömungskanal

Publications (2)

Publication Number Publication Date
FR2485620A1 FR2485620A1 (fr) 1981-12-31
FR2485620B1 true FR2485620B1 (fr) 1985-12-27

Family

ID=6105244

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8111803A Expired FR2485620B1 (fr) 1980-06-24 1981-06-16 Dispositif pour reduire les pertes secondaires dans un conduit d'ecoulement de turbomachine muni d'aubages

Country Status (5)

Country Link
US (1) US4420288A (fr)
JP (1) JPS5738601A (fr)
DE (1) DE3023466C2 (fr)
FR (1) FR2485620B1 (fr)
GB (1) GB2079399B (fr)

Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3202855C1 (de) * 1982-01-29 1983-03-31 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Verminderung von Sekundaerstroemungsverlusten in einem beschaufelten Stroemungskanal
US4958985A (en) * 1989-03-01 1990-09-25 Westinghouse Electric Corp. Performance low pressure end blading
US5215439A (en) * 1991-01-15 1993-06-01 Northern Research & Engineering Corp. Arbitrary hub for centrifugal impellers
EP0567589A1 (fr) * 1991-01-15 1993-11-03 NORTHERN RESEARCH & ENGINEERING CORPORATION Moyeu arbitraire pour roue a aubes
GB2281356B (en) * 1993-08-20 1997-01-29 Rolls Royce Plc Gas turbine engine turbine
DE9316009U1 (de) * 1993-10-20 1994-01-13 Moser, Josef, 85435 Erding Oberfläche eines fluidumströmten Körpers
DE19650656C1 (de) * 1996-12-06 1998-06-10 Mtu Muenchen Gmbh Turbomaschine mit transsonischer Verdichterstufe
WO1998044240A1 (fr) * 1997-04-01 1998-10-08 Siemens Aktiengesellschaft Structure superficielle pour la paroi d'un canal d'ecoulement ou d'une aube de turbine
GB9823840D0 (en) 1998-10-30 1998-12-23 Rolls Royce Plc Bladed ducting for turbomachinery
US6283705B1 (en) * 1999-02-26 2001-09-04 Allison Advanced Development Company Variable vane with winglet
US6419446B1 (en) * 1999-08-05 2002-07-16 United Technologies Corporation Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engine
US6511294B1 (en) 1999-09-23 2003-01-28 General Electric Company Reduced-stress compressor blisk flowpath
US6524070B1 (en) 2000-08-21 2003-02-25 General Electric Company Method and apparatus for reducing rotor assembly circumferential rim stress
US6471474B1 (en) 2000-10-20 2002-10-29 General Electric Company Method and apparatus for reducing rotor assembly circumferential rim stress
US6794473B2 (en) 2001-05-01 2004-09-21 Nippon Shokubai Co., Ltd. Acrylic acid (salt) polymer, its production process and uses
US6672832B2 (en) * 2002-01-07 2004-01-06 General Electric Company Step-down turbine platform
US7134842B2 (en) * 2004-12-24 2006-11-14 General Electric Company Scalloped surface turbine stage
US7189055B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Coverplate deflectors for redirecting a fluid flow
US7244104B2 (en) * 2005-05-31 2007-07-17 Pratt & Whitney Canada Corp. Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine
US7189056B2 (en) * 2005-05-31 2007-03-13 Pratt & Whitney Canada Corp. Blade and disk radial pre-swirlers
US7874794B2 (en) * 2006-03-21 2011-01-25 General Electric Company Blade row for a rotary machine and method of fabricating same
FR2907519B1 (fr) * 2006-10-20 2011-12-16 Snecma Nageoire de plateforme de soufflante
JP5283855B2 (ja) * 2007-03-29 2013-09-04 株式会社Ｉｈｉ ターボ機械の壁、及びターボ機械
WO2009019282A2 (fr) * 2007-08-06 2009-02-12 Alstom Technology Ltd Installation de turbine à gaz
DE102008031789A1 (de) * 2008-07-04 2010-01-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Vorrichtung zur Beeinflussung von Sekundärströmungen bei einer Turbomaschine
DE102008060424A1 (de) * 2008-12-04 2010-06-10 Rolls-Royce Deutschland Ltd & Co Kg Strömungsmaschine mit Seitenwand-Grenzschicht-Barriere
EP2194231A1 (fr) * 2008-12-05 2010-06-09 Siemens Aktiengesellschaft Diffuseur annulaire pour une turbomachine axiale
EP2224096A1 (fr) * 2009-02-27 2010-09-01 Alstom Technology Ltd Turbine à vapeur et procédé pour extraire de l'humidité d'une turbine à vapeur
US8182204B2 (en) * 2009-04-24 2012-05-22 Pratt & Whitney Canada Corp. Deflector for a gas turbine strut and vane assembly
US8100643B2 (en) * 2009-04-30 2012-01-24 Pratt & Whitney Canada Corp. Centrifugal compressor vane diffuser wall contouring
US8517686B2 (en) * 2009-11-20 2013-08-27 United Technologies Corporation Flow passage for gas turbine engine
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
US8926267B2 (en) 2011-04-12 2015-01-06 Siemens Energy, Inc. Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling
JP2012233406A (ja) 2011-04-28 2012-11-29 Hitachi Ltd ガスタービン静翼
CN202937553U (zh) * 2011-07-09 2013-05-15 拉姆金动力系统有限责任公司 涡流发生器及使用其的飞机、装置、陆地车辆、风力涡轮机和涡流发生器阵列
US9267386B2 (en) 2012-06-29 2016-02-23 United Technologies Corporation Fairing assembly
WO2014028056A1 (fr) 2012-08-17 2014-02-20 United Technologies Corporation Surface profilée de chemin d'écoulement
WO2014041619A1 (fr) * 2012-09-12 2014-03-20 株式会社 日立製作所 Turbine à gaz
WO2014105102A1 (fr) 2012-12-28 2014-07-03 United Technologies Corporation Plate-forme à bords courbes adjacente à l'extrados d'un profil aérodynamique
WO2014163681A1 (fr) 2013-03-10 2014-10-09 Fulayter Roy D Turbines à gaz et procédé correspondant
EP2835499B1 (fr) * 2013-08-06 2019-10-09 MTU Aero Engines GmbH Grille d'aubes et turbomachine associée
FR3014943B1 (fr) * 2013-12-18 2019-03-29 Safran Aircraft Engines Piece de turbomachine a surface non-axisymetrique
FR3059735B1 (fr) * 2016-12-05 2020-09-25 Safran Aircraft Engines Piece de turbomachine a surface non-axisymetrique
EP3404210B1 (fr) * 2017-05-15 2024-07-31 MTU Aero Engines AG Segment de grille d'aubes d'une turbomachine avec paroi de plateforme non-axisymétrique , grille d'aubes, canal d'aube, plateforme, turbomachine associés
US10480333B2 (en) * 2017-05-30 2019-11-19 United Technologies Corporation Turbine blade including balanced mateface condition
US10577955B2 (en) 2017-06-29 2020-03-03 General Electric Company Airfoil assembly with a scalloped flow surface
DE102017122524A1 (de) * 2017-09-28 2019-03-28 Abb Turbo Systems Ag Diffusor für einen Verdichter
EP3608505B1 (fr) 2018-08-08 2021-06-23 General Electric Company Turbine intégrant des clôtures de paroi terminale
IT202100002240A1 (it) 2021-02-02 2022-08-02 Gen Electric Motore a turbine con palette a flusso trasversale ridotto
FR3139595A1 (fr) * 2022-09-09 2024-03-15 Safran Aube directrice destinée à être fixée sur une virole de stator d’un moteur à turbine à gaz

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2918254A (en) * 1954-05-10 1959-12-22 Hausammann Werner Turborunner
US3039736A (en) * 1954-08-30 1962-06-19 Pon Lemuel Secondary flow control in fluid deflecting passages
GB944166A (en) * 1960-03-02 1963-12-11 Werner Hausammann Rotor for turbines or compressors
FR1442526A (fr) * 1965-05-07 1966-06-17 Rateau Soc Perfectionnements aux canaux courbes parcourus par un gaz ou une vapeur
US3578264A (en) * 1968-07-09 1971-05-11 Battelle Development Corp Boundary layer control of flow separation and heat exchange
DE1937395A1 (de) * 1969-07-23 1971-02-11 Dettmering Prof Dr Ing Wilhelm Gitter zur Vermeidung der Sekundaerstroemung
DE2135286A1 (de) * 1971-07-15 1973-01-25 Wilhelm Prof Dr Ing Dettmering Lauf- und leitradgitter fuer turbomaschinen
JPS5254808A (en) * 1975-10-31 1977-05-04 Hitachi Ltd Blade arrangement device of fluid machine
JPS5267404A (en) * 1975-12-01 1977-06-03 Hitachi Ltd Blades structure
US4135857A (en) * 1977-06-09 1979-01-23 United Technologies Corporation Reduced drag airfoil platforms
JPS54151707A (en) * 1978-05-22 1979-11-29 Hitachi Ltd Turbine blade lattice structure
FR2432608A1 (fr) * 1978-07-31 1980-02-29 Alsthom Atlantique Grille d'aubes pour turbine ou compresseur
GB2042675A (en) * 1979-02-15 1980-09-24 Rolls Royce Secondary Flow Control in Axial Fluid Flow Machine

Also Published As

Publication number Publication date
DE3023466C2 (de) 1982-11-25
GB2079399A (en) 1982-01-20
FR2485620A1 (fr) 1981-12-31
DE3023466A1 (de) 1982-01-07
GB2079399B (en) 1984-05-10
US4420288A (en) 1983-12-13
JPS6243042B2 (fr) 1987-09-11
JPS5738601A (en) 1982-03-03

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Legal Events

Date Code Title Description
ST Notification of lapse