ES8504330A1 - Un alabe de superficie aerodinamica para un rotor refrigerado de primera etapa de una turbina de combustion terrestre - Google Patents

Un alabe de superficie aerodinamica para un rotor refrigerado de primera etapa de una turbina de combustion terrestre

Info

Publication number
ES8504330A1
ES8504330A1 ES526667A ES526667A ES8504330A1 ES 8504330 A1 ES8504330 A1 ES 8504330A1 ES 526667 A ES526667 A ES 526667A ES 526667 A ES526667 A ES 526667A ES 8504330 A1 ES8504330 A1 ES 8504330A1
Authority
ES
Spain
Prior art keywords
rotor
alabe
combustion turbine
aerodynamic surface
land
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
ES526667A
Other languages
English (en)
Other versions
ES526667A0 (es
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.)
Westinghouse Electric Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of ES8504330A1 publication Critical patent/ES8504330A1/es
Publication of ES526667A0 publication Critical patent/ES526667A0/es
Granted 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/301—Cross-sectional characteristics
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

ALABE DE SUPERFICIE AERODINAMICA PARA UN MOTOR REFRIGERADO DE PRIMERA ETAPA DE UNA TURBINA DE COMBUSTION TERRESTRE.CONSTA DE UNA PORCION AERODINAMICA (21) QUE TIENE UN BORDE DE ENTRADA (22) Y UN BORDE DE SALIDA (24) CON SUPERFICIES CONCAVA (26) Y CONVEXA (28) ENTRE ELLOS; UNA PORCION DE RAIZ (27); Y UNA PORCION DE PLATAFORMA (23). LA PORCION AERODINAMICA INCLUYE: UNA ZONA TRANSVERSAL GRADUALMENTE DECRECIENTE CON RADIO CRECIENTE; UN GROSOR TRANSVERSAL MAXIMO QUE DISMINUYE ENTRE LOS LADOS CONVEXO Y CONCAVO CON RADIO CRECIENTE DESDE 1,0L (2,54 CM) A 0,78L; UNA ANCHURA TRANSVERSAL QUE DISMINUYE CON RADIO CRECIENTE DESDE 3,853L HASTA 3,240L; UNA CUERDA QUE DISMINUYE CON RADIO CRECIENTE DESDE 4,051L A 3,965L; TENIENDO EL BORDE DE ENTRADA UN RADIO QUE DISMINUYE CON RADIO CRECIENTE DESDE 0,141L HASTA 0,102L.
ES526667A 1982-10-22 1983-10-21 Un alabe de superficie aerodinamica para un rotor refrigerado de primera etapa de una turbina de combustion terrestre Granted ES526667A0 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US43610282A 1982-10-22 1982-10-22

Publications (2)

Publication Number Publication Date
ES8504330A1 true ES8504330A1 (es) 1985-04-16
ES526667A0 ES526667A0 (es) 1985-04-16

Family

ID=23731117

Family Applications (1)

Application Number Title Priority Date Filing Date
ES526667A Granted ES526667A0 (es) 1982-10-22 1983-10-21 Un alabe de superficie aerodinamica para un rotor refrigerado de primera etapa de una turbina de combustion terrestre

Country Status (12)

Country Link
EP (1) EP0112003B1 (es)
JP (1) JPS59131704A (es)
KR (1) KR910010034B1 (es)
AU (1) AU568313B2 (es)
BR (1) BR8305902A (es)
CA (1) CA1210334A (es)
DE (1) DE3377925D1 (es)
ES (1) ES526667A0 (es)
IE (1) IE54653B1 (es)
IL (1) IL69920A (es)
IN (1) IN158893B (es)
MX (1) MX157076A (es)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5088894A (en) * 1990-05-02 1992-02-18 Westinghouse Electric Corp. Turbomachine blade fastening
US5286169A (en) * 1992-12-15 1994-02-15 General Electric Company Bucket for the next-to-last stage of a steam turbine
US5352092A (en) * 1993-11-24 1994-10-04 Westinghouse Electric Corporation Light weight steam turbine blade
US5980209A (en) * 1997-06-27 1999-11-09 General Electric Co. Turbine blade with enhanced cooling and profile optimization
US6461110B1 (en) * 2001-07-11 2002-10-08 General Electric Company First-stage high pressure turbine bucket airfoil
US6503054B1 (en) * 2001-07-13 2003-01-07 General Electric Company Second-stage turbine nozzle airfoil
US6461109B1 (en) * 2001-07-13 2002-10-08 General Electric Company Third-stage turbine nozzle airfoil
WO2003006797A1 (en) * 2001-07-13 2003-01-23 General Electric Company Second-stage turbine nozzle airfoil
WO2007141596A2 (en) 2005-12-29 2007-12-13 Rolls-Royce Power Engineering Plc Turbine nozzle blade airfoil geometry
WO2008090394A2 (en) 2005-12-29 2008-07-31 Rolls-Royce Power Engineering Plc Second stage turbine airfoil
WO2007085912A2 (en) 2005-12-29 2007-08-02 Rolls-Royce Power Engineering Plc Airfoil for a first stage nozzle guide vane
US7722329B2 (en) 2005-12-29 2010-05-25 Rolls-Royce Power Engineering Plc Airfoil for a third stage nozzle guide vane
US7648340B2 (en) 2005-12-29 2010-01-19 Rolls-Royce Power Engineering Plc First stage turbine airfoil
US7632072B2 (en) 2005-12-29 2009-12-15 Rolls-Royce Power Engineering Plc Third stage turbine airfoil
DE102008031781B4 (de) * 2008-07-04 2020-06-10 Man Energy Solutions Se Schaufelgitter für eine Strömungsmaschine und Strömungsmaschine mit einem solchen Schaufelgitter
JP5946707B2 (ja) * 2012-07-06 2016-07-06 三菱日立パワーシステムズ株式会社 軸流タービン動翼
FR3089550B1 (fr) * 2018-12-11 2021-01-22 Safran Aircraft Engines Aube de turbomachine a loi d’epaisseur maximale a forte marge au flottement
FR3089553B1 (fr) * 2018-12-11 2021-01-22 Safran Aircraft Engines Aube de turbomachine a loi de fleche a forte marge au flottement
JP2025165430A (ja) * 2024-04-23 2025-11-05 三菱重工業株式会社 軸流圧縮機、及びその動翼

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1548613A (en) * 1924-03-21 1925-08-04 Aeg Elastic-fluid turbine
GB686807A (en) * 1950-11-14 1953-01-28 British Thomson Houston Co Ltd Improvements in and relating to blades for compressors and the like
US4111604A (en) * 1976-07-12 1978-09-05 General Electric Company Bucket tip construction for open circuit liquid cooled turbines

Also Published As

Publication number Publication date
JPS59131704A (ja) 1984-07-28
IN158893B (es) 1987-02-14
KR840006397A (ko) 1984-11-29
IL69920A (en) 1988-10-31
MX157076A (es) 1988-10-26
CA1210334A (en) 1986-08-26
AU1996383A (en) 1984-05-03
BR8305902A (pt) 1984-05-29
KR910010034B1 (ko) 1991-12-10
AU568313B2 (en) 1987-12-24
DE3377925D1 (en) 1988-10-13
JPH0312641B2 (es) 1991-02-20
IL69920A0 (en) 1984-01-31
IE54653B1 (en) 1989-12-20
EP0112003B1 (en) 1988-09-07
IE832335L (en) 1984-04-22
EP0112003A1 (en) 1984-06-27
ES526667A0 (es) 1985-04-16

Similar Documents

Publication Publication Date Title
IE832335L (en) Rotor blade
SE8904237D0 (sv) Boltless balance weight for turbine rotors
IT8522246A0 (it) Perfezionamenti relativi a palette per turbine a combustione terrestri e marine.
GB2028928B (en) Aerofoil blade for a gas turbine engine
SE8305993L (sv) Motroterande kraftturbin
GB2036885B (en) Maintaining vane clearance in gas turbine engine
SE8601928L (sv) Gasturbinmotorer
GB2043796B (en) Bladed rotor for gas turbine engine
CA2130628A1 (en) Steam turbine blade
JPS53125518A (en) Cooling type rotor blade for gas turbine engine
IT8520944A0 (it) Sistema di ritegno di pale, specialmente di pale di compressori di turbomotori a gas.
DE68900653D1 (de) Fabrikationsmethode einer luftgekuehlten gasturbinenschaufel.
DE3876768D1 (de) Axial durchstroemtes laufschaufelgitter fuer verdichter oder turbinen.
IT8521956A0 (it) Metodo per la produzione di palette per turbine a combustione aventi una parte monocristallina.
AU574050B2 (en) Turbine blade with integral shroud
GB8302880D0 (en) Combustion turbine single airfoil stator vane structure
FR2706528B1 (fr) Plate-forme séparée inter-aube de disque ailette de rotor de turbomachine.
GB1266505A (es)
IT1193595B (it) Prgano di comando,in particolare per la messa in marcia di turbine di servizio a aria per velivoli
GB2030233B (en) Gas turbine engine blade
ES2008170A6 (es) Alabe de rotor para turbina de vapor
IT7925758A0 (it) Paletta rotorica e direttrice ricurva per motore a turbina a gas e relativo metodo di fabbricazione.
SARAVANAMUTTO et al. Prediction of fouled compressor performance using stage stacking techniques
MX157531A (es) Mejoras en alabe de rotor para una turbina de combustion
JPS55123303A (en) Gas turbine engine blade rotor