MX9101073A - Rejilla de aleta para turbomotor. - Google Patents

Rejilla de aleta para turbomotor.

Info

Publication number
MX9101073A
MX9101073A MX9101073A MX9101073A MX9101073A MX 9101073 A MX9101073 A MX 9101073A MX 9101073 A MX9101073 A MX 9101073A MX 9101073 A MX9101073 A MX 9101073A MX 9101073 A MX9101073 A MX 9101073A
Authority
MX
Mexico
Prior art keywords
blade
slit
turbomotor
turbomachine
ceiling
Prior art date
Application number
MX9101073A
Other languages
English (en)
Inventor
Michel Vicent De Paul
Francois Detanne
Original Assignee
Alsthom Gec
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 Alsthom Gec filed Critical Alsthom Gec
Publication of MX9101073A publication Critical patent/MX9101073A/es

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
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • F04D29/682Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid extraction
    • 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
    • Y10S415/914Device to control boundary layer

Landscapes

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

Abstract

Se describe una rejilla de álabes para turbomáquina o turbomotor que lleva álabes (A,B) colocados entre un piso y un techo y cuyo piso y/o techo están provistos de una abertura de aspiración (4,4') en la vecindad de al menos ciertos álabes (A), dicha abertura (4,4') tiene una primera extremidad (6) colocada a lo largo del extradós en un dominio del álabe (A) activo en la zona de curvatura máxima (7) en el cuello (8) del canal (3) entre este álabe (A) y el álabe vecino (B), caracterizado porque dicha abertura (4,4') está orientado según una línea isobárica y a una longitud tal que la segunda extremidad (9) es apartada del extradós del álabe (A) una distancia comprendida entra una cuarta parte y la mitad de la anchura del cuello (8) del canal (3).
MX9101073A 1990-09-13 1991-09-12 Rejilla de aleta para turbomotor. MX9101073A (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9011336A FR2666846B1 (fr) 1990-09-13 1990-09-13 Grille d'aubes pour turbomachine munie de fentes d'aspiration dans le plafond et/ou dans le plancher et turbomachine comportant ces grilles.

Publications (1)

Publication Number Publication Date
MX9101073A true MX9101073A (es) 1994-06-30

Family

ID=9400301

Family Applications (1)

Application Number Title Priority Date Filing Date
MX9101073A MX9101073A (es) 1990-09-13 1991-09-12 Rejilla de aleta para turbomotor.

Country Status (10)

Country Link
US (1) US5232338A (es)
EP (1) EP0475329B1 (es)
JP (1) JPH04279701A (es)
CN (1) CN1060891A (es)
AT (1) ATE114780T1 (es)
CS (1) CS281991A3 (es)
DE (1) DE69105418T2 (es)
FR (1) FR2666846B1 (es)
MX (1) MX9101073A (es)
ZA (1) ZA917326B (es)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2675536B1 (fr) * 1991-04-19 1994-12-09 Alsthom Gec Turbine a action a rotor tambour et perfectionnement a ces turbines.
US5632598A (en) * 1995-01-17 1997-05-27 Dresser-Rand Shrouded axial flow turbo machine utilizing multiple labrinth seals
DE19620828C1 (de) * 1996-05-23 1997-09-04 Siemens Ag Turbinenwelle sowie Verfahren zur Kühlung einer Turbinenwelle
US6004095A (en) * 1996-06-10 1999-12-21 Massachusetts Institute Of Technology Reduction of turbomachinery noise
US5904470A (en) * 1997-01-13 1999-05-18 Massachusetts Institute Of Technology Counter-rotating compressors with control of boundary layers by fluid removal
EP0894944A1 (de) * 1997-07-29 1999-02-03 Siemens Aktiengesellschaft Turbinenbeschaufelung
ATE371097T1 (de) 1998-02-26 2007-09-15 Allison Advanced Dev Co Zapfsystem für eine kompressorwand sowie betriebsverfahren
US6595743B1 (en) * 1999-07-26 2003-07-22 Impsa International Inc. Hydraulic seal for rotary pumps
US6632069B1 (en) * 2001-10-02 2003-10-14 Oleg Naljotov Step of pressure of the steam and gas turbine with universal belt
US20040101410A1 (en) * 2001-10-02 2004-05-27 Oleg Naljotov Axial flow fluid machine
US6682301B2 (en) * 2001-10-05 2004-01-27 General Electric Company Reduced shock transonic airfoil
GB0200992D0 (en) * 2002-01-17 2002-03-06 Rolls Royce Plc Gas turbine cooling system
WO2004099572A1 (en) * 2003-04-18 2004-11-18 Oleg Naljotov Steam/gas turbine pressure stage with universal shroud
US20070069477A1 (en) * 2003-06-20 2007-03-29 Elliott Company Stepped labyrinth damper seal
WO2004113771A2 (en) * 2003-06-20 2004-12-29 Elliott Company Hybrid abradable labyrinth damper seal
JP4346412B2 (ja) 2003-10-31 2009-10-21 株式会社東芝 タービン翼列装置
DE10355241A1 (de) * 2003-11-26 2005-06-30 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Fluidzufuhr
DE10355240A1 (de) * 2003-11-26 2005-07-07 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Fluidentnahme
DE102007027427A1 (de) * 2007-06-14 2008-12-18 Rolls-Royce Deutschland Ltd & Co Kg Schaufeldeckband mit Überstand
DE102008029605A1 (de) * 2008-06-23 2009-12-24 Rolls-Royce Deutschland Ltd & Co Kg Schaufeldeckband mit Durchlass
FR2958694B1 (fr) * 2010-04-07 2014-04-18 Snecma Compresseur de moteur, en particulier de turboreacteur d'aeronef, muni d'un systeme de prelevement d'air
CN102364098A (zh) * 2011-11-18 2012-02-29 三一电气有限责任公司 一种风力发电机组及其叶片
EP2713009B1 (en) * 2012-09-26 2015-03-11 Alstom Technology Ltd Cooling method and system for cooling blades of at least one blade row in a rotary flow machine
CN109413711B (zh) * 2018-10-17 2021-02-05 中国运载火箭技术研究院 一种飞行器协同信息网络协议栈
US11674406B2 (en) * 2021-08-06 2023-06-13 Pratt & Whitney Canada Corp. Variable gap between impeller rotor and static structure

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS501646B1 (es) * 1970-07-11 1975-01-20
DE2135286A1 (de) * 1971-07-15 1973-01-25 Wilhelm Prof Dr Ing Dettmering Lauf- und leitradgitter fuer turbomaschinen
FR2166494A5 (es) * 1971-12-27 1973-08-17 Onera (Off Nat Aerospatiale)
JPS5254809A (en) * 1975-10-31 1977-05-04 Hitachi Ltd Axial-flow fluid machine construction
JPS5254807A (en) * 1975-10-31 1977-05-04 Hitachi Ltd Axial-flow fluid machine
FR2438157A1 (fr) * 1978-10-05 1980-04-30 Alsthom Atlantique Grille d'aubes pour turbine ou compresseur
FR2438155A1 (fr) * 1978-10-05 1980-04-30 Alsthom Atlantique Grille d'aubes pour turbine ou compresseur et turbine ou compresseur comportant une telle grille d'aubes
DE2845094A1 (de) * 1978-10-17 1980-05-08 Freudenberg Carl Fa Greifvorrichtung
FR2473290A1 (fr) * 1980-01-14 1981-07-17 Treboul Douarnenez Ctre Cure M Plateau de relaxation et table comportant un tel plateau
JPS5752603A (en) * 1980-09-17 1982-03-29 Toshiba Corp Leakage preventing device in turbine
SU1015082A1 (ru) * 1981-07-13 1983-04-30 Московский Ордена Ленина И Ордена Октябрьской Революции Энергетический Институт Многоступенчата парова турбина
SU1159970A1 (ru) * 1982-12-31 1985-06-07 Всесоюзный Дважды Ордена Трудового Красного Знамени Теплотехнический Научно-Исследовательский Институт Им.Ф.Э.Дзержинского Ступень турбомашины

Also Published As

Publication number Publication date
FR2666846A1 (fr) 1992-03-20
DE69105418T2 (de) 1995-04-20
CN1060891A (zh) 1992-05-06
JPH04279701A (ja) 1992-10-05
CS281991A3 (en) 1992-03-18
US5232338A (en) 1993-08-03
EP0475329A2 (fr) 1992-03-18
ZA917326B (en) 1992-05-27
EP0475329A3 (en) 1992-06-03
DE69105418D1 (de) 1995-01-12
EP0475329B1 (fr) 1994-11-30
FR2666846B1 (fr) 1992-10-16
ATE114780T1 (de) 1994-12-15

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