MX166759B - Turbomaquina con partes secundarias reducidas - Google Patents

Turbomaquina con partes secundarias reducidas

Info

Publication number
MX166759B
MX166759B MX025748A MX2574891A MX166759B MX 166759 B MX166759 B MX 166759B MX 025748 A MX025748 A MX 025748A MX 2574891 A MX2574891 A MX 2574891A MX 166759 B MX166759 B MX 166759B
Authority
MX
Mexico
Prior art keywords
disc
blades
bank
orifices
diaphragm
Prior art date
Application number
MX025748A
Other languages
English (en)
Inventor
Fancois 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 MX166759B publication Critical patent/MX166759B/es

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)
  • Exhaust Gas After Treatment (AREA)
  • Diaphragms For Cameras (AREA)

Abstract

La presente invención se refiere a un cuerpo o etapa de turbina que lleva una rejilla de álabes fijos, solidarios con el estator de la turbina, que soporta un diafragma seguido de una rejilla de álabes móviles montada sobre un disco solidario con el rotor de la turbina, dicha rejilla de álabes móviles lleva en su cúspide una guarnición de hermeticidad constituída de varias cámaras, el disco lleva orificios de aspiración que desembocan en el espacio entre el diafragma y el disco y colocados en la vecindad de la parte periférica del disco, el cuerpo o etapa de turbina está caracterizada en que dichos orificios de aspiración estan conectados por canalizaciones que atraviesan al menos ciertos álabes móviles hasta los orificios de salida que desembocan en la cúspide de estos álabes, debajo de la guarnición de hermeticidad o en una cámara de la misma.
MX025748A 1990-05-14 1991-05-10 Turbomaquina con partes secundarias reducidas MX166759B (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
MX166759B true MX166759B (es) 1993-02-02

Family

ID=9396584

Family Applications (1)

Application Number Title Priority Date Filing Date
MX025748A MX166759B (es) 1990-05-14 1991-05-10 Turbomaquina con partes 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
UA81314C2 (en) * 2003-04-18 2007-12-25 Steam/gas turbine with shroud
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
ATE100177T1 (de) 1994-01-15
DE69100968T2 (de) 1994-05-05
FR2661944B1 (fr) 1994-06-10
US5167486A (en) 1992-12-01
ZA913635B (en) 1992-02-26
CZ279114B6 (cs) 1995-01-18
CN1057504A (zh) 1992-01-01
FR2661944A1 (fr) 1991-11-15
DK0457240T3 (da) 1994-05-09
CS139591A3 (en) 1992-01-15
EP0457240A1 (fr) 1991-11-21
DE69100968D1 (de) 1994-02-24
ES2049061T3 (es) 1994-04-01
JPH04228807A (ja) 1992-08-18
EP0457240B1 (fr) 1994-01-12

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