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ES2049061T3 - Bancal de turbomaquina con perdidas secundarias reducidas. - Google Patents

Bancal de turbomaquina con perdidas secundarias reducidas.

Info

Publication number
ES2049061T3
ES2049061T3 ES91107716T ES91107716T ES2049061T3 ES 2049061 T3 ES2049061 T3 ES 2049061T3 ES 91107716 T ES91107716 T ES 91107716T ES 91107716 T ES91107716 T ES 91107716T ES 2049061 T3 ES2049061 T3 ES 2049061T3
Authority
ES
Spain
Prior art keywords
bank
disc
blades
orifices
diaphragm
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
ES91107716T
Other languages
English (en)
Inventor
Francois Detanne
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.)
Alstom Holdings SA
Original Assignee
GEC Alsthom SA
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 GEC Alsthom SA filed Critical GEC Alsthom SA
Application granted granted Critical
Publication of ES2049061T3 publication Critical patent/ES2049061T3/es
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
    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • 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)
  • 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)
  • Supercharger (AREA)
  • Diaphragms For Cameras (AREA)
  • Exhaust Gas After Treatment (AREA)

Abstract

ESCALON DE TURBINA QUE COMPRENDE UNA REJILLA DE ALABES FIJAS (1) SOLIDARIA DEL ESTATOR (3) DE LA TURBINA QUE SOPORTA UN DIAFRAGMA SEGUIDA DE UNA REJILLA DE ALABES MOVILES (7) MONTADA SOBRE UN DISCO (9) SOLIDARIO DEL ROTOR (6) DE LA TURBINA, COMPRENDIENDO DICHA REJILLA DE ALABES MOVILES EN SU PARTE SUPERIOR UN HERRAJE DE ESTANQUEIDAD (10) CONSTITUIDO POR VARIAS RAMAS (11). EL DISCO (9) COMPRENDE ORIFICIOS DE ASPIRACION (16) QUE DESEMBOCAN EN EL ESPACIO QUE HAY ENTRE EL DIAFRAGMA (4) Y EL DISCO Y DISPUESTOS CERCA DE LA PARTE PERIFERICA DEL DISCO (9). LOS ORIFICIOS DE ASPIRACION (16) ESTAN CONECTADOS POR CANALIZACIONES (17) QUE ATRAVIESAN AL MENOS ALGUNOS ALABES MOVILES (8) HASTA UNOS ORIFICIOS DE SALIDA (18) QUE DESEMBOCAN EN LA PARTE SUPERIOR DE ESTOS ALABES (8) POR DEBAJO DEL HERRAJE DE ESTANQUEIDAD (10) O EN UNA CAMARA DE ESTE (11). LA CIRCULACION PERTURBADA A LOS PIES DE LOS ALABES FIJOS (2) Y LA CIRCULACION DE FUGA ENTRE EL DIAFRAGMA (4) Y EL ROTOR (6) SON ASPIRADOS POR LOS ORIFICIOS (16), LO QUE MEJORA EL RENDIMIENTO.
ES91107716T 1990-05-14 1991-05-13 Bancal de turbomaquina con perdidas secundarias reducidas. Expired - Lifetime ES2049061T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR909005991A FR2661944B1 (fr) 1990-05-14 1990-05-14 Etage de turbomachine avec pertes secondaires reduites.

Publications (1)

Publication Number Publication Date
ES2049061T3 true ES2049061T3 (es) 1994-04-01

Family

ID=9396584

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91107716T Expired - Lifetime ES2049061T3 (es) 1990-05-14 1991-05-13 Bancal de turbomaquina con perdidas secundarias reducidas.

Country Status (12)

Country Link
US (1) US5167486A (es)
EP (1) EP0457240B1 (es)
JP (1) JPH04228807A (es)
CN (1) CN1057504A (es)
AT (1) ATE100177T1 (es)
CZ (1) CZ279114B6 (es)
DE (1) DE69100968T2 (es)
DK (1) DK0457240T3 (es)
ES (1) ES2049061T3 (es)
FR (1) FR2661944B1 (es)
MX (1) MX166759B (es)
ZA (1) ZA913635B (es)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CZ406592A3 (en) * 1992-01-08 1993-08-11 Alsthom Gec Drum rotor for steam action turbine and steam action turbine comprising such rotor
GB0200992D0 (en) * 2002-01-17 2002-03-06 Rolls Royce Plc Gas turbine cooling system
EP1623097A4 (en) * 2003-04-18 2012-06-27 Oleg Naljotov STEAM / GAS TURBINE PRESSURE STAGE WITH UNIVERSAL COVER
EP1767746A1 (en) * 2005-09-22 2007-03-28 Siemens Aktiengesellschaft Turbine blade/vane and turbine section comprising a plurality of such turbine blades/vanes
GB0901473D0 (en) * 2009-01-30 2009-03-11 Rolls Royce Plc An axial-flow turbo machine
JP5404187B2 (ja) * 2009-05-29 2014-01-29 三菱重工業株式会社 端壁部材及びガスタービン
DE102009040758A1 (de) * 2009-09-10 2011-03-17 Mtu Aero Engines Gmbh Umlenkvorrichtung für einen Leckagestrom in einer Gasturbine und Gasturbine
US8545170B2 (en) * 2009-10-27 2013-10-01 General Electric Company Turbo machine efficiency equalizer system
WO2012052740A1 (en) * 2010-10-18 2012-04-26 University Of Durham Sealing device for reducing fluid leakage in turbine apparatus
US10107115B2 (en) * 2013-02-05 2018-10-23 United Technologies Corporation Gas turbine engine component having tip vortex creation feature
US9032733B2 (en) 2013-04-04 2015-05-19 General Electric Company Turbomachine system with direct header steam injection, related control system and program product
CN104896100B (zh) * 2015-05-25 2017-06-13 沈阳航空航天大学 一种降低预旋抑制气流失稳力的反旋流梳齿密封结构
CZ2022355A3 (cs) * 2022-08-25 2023-10-25 Doosan Ĺ koda Power s.r.o. Turbínová sestava axiální turbíny

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2945671A (en) * 1955-02-10 1960-07-19 Rolls Royce Bladed rotor constructions for fluid machines
GB855058A (en) * 1957-02-22 1960-11-30 Rolls Royce Improvements in or relating to bladed rotor or stator constructions for axial-flow fluid machines for example for compressors or turbines of gas-turbine engines
FR1245518A (fr) * 1957-04-19 1960-11-10 Perfectionnements apportés aux turbines à fluide gazeux chaud
FR1194770A (fr) * 1958-04-16 1959-11-12 Rateau Soc Perfectionnements au refroidissement des rotors de turbines à vapeur et à gaz
DE1159970B (de) * 1961-10-30 1963-12-27 Licentia Gmbh Kuehlschrankthermostat mit halbautomatischer Abtauvorrichtung
BE624309A (es) * 1961-11-02 1963-02-15
US3904307A (en) * 1974-04-10 1975-09-09 United Technologies Corp Gas generator turbine cooling scheme
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
JPS6014161A (ja) * 1983-07-06 1985-01-24 Ngk Spark Plug Co Ltd 空燃比センサ
US4761116A (en) * 1987-05-11 1988-08-02 General Electric Company Turbine blade with tip vent
US4830575A (en) * 1988-02-08 1989-05-16 Dresser-Rand Company Spiral grooves in a turbine rotor

Also Published As

Publication number Publication date
FR2661944A1 (fr) 1991-11-15
DE69100968T2 (de) 1994-05-05
JPH04228807A (ja) 1992-08-18
DK0457240T3 (da) 1994-05-09
US5167486A (en) 1992-12-01
CZ279114B6 (cs) 1995-01-18
EP0457240B1 (fr) 1994-01-12
MX166759B (es) 1993-02-02
DE69100968D1 (de) 1994-02-24
FR2661944B1 (fr) 1994-06-10
ZA913635B (en) 1992-02-26
ATE100177T1 (de) 1994-01-15
CN1057504A (zh) 1992-01-01
EP0457240A1 (fr) 1991-11-21
CS139591A3 (en) 1992-01-15

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