ES2024210A6 - Alabe de extremidad de baja presion presion para un turbina de vapor de baja presion. - Google Patents

Alabe de extremidad de baja presion presion para un turbina de vapor de baja presion.

Info

Publication number
ES2024210A6
ES2024210A6 ES9001190A ES9001190A ES2024210A6 ES 2024210 A6 ES2024210 A6 ES 2024210A6 ES 9001190 A ES9001190 A ES 9001190A ES 9001190 A ES9001190 A ES 9001190A ES 2024210 A6 ES2024210 A6 ES 2024210A6
Authority
ES
Spain
Prior art keywords
low pressure
alabe
steam turbine
extremity
wires
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
ES9001190A
Other languages
English (en)
Inventor
Ashok T Patel
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 ES2024210A6 publication Critical patent/ES2024210A6/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
    • 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
    • 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
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/02—Formulas of curves

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

ALABE DE EXTREMIDAD DE BAJA PRESION PARA UNA TURBINA DE VAPOR DE BAJA PRESION. SE TRATA CONCRETAMENTE DE UN SISTEMA SUSTITUTIVO DE ALABES DE EXTREMIDAD DE BAJA PRESION PARA UNA TURBINA DE VAPOR DE CENTRAL ELECTRICA, QUE TIENE UNA LONGITUD AMPLIADA EN COMPARACION CON EL SISTEMA DE ALABES DE EXTREMIDAD DEL EQUIPO ORIGINARIO, DANDO UN MAYOR RENDIMIENTO, Y EN DONDE EL SISTEMA DE ALABES LLEVA INCORPORADAS UNAS AREAS PLANAS AMPLIADAS EN EL BORDE DE SALIDA DEL ALABE PARA MEJORAR LAS CARACTERISTICAS DE FLUJO Y REDUCIR PERDIDAS. SE USA UNA DISTRIBUCION DE MASAS PARA <SINTONIZAR> EL ALABE EVITANDO LA COINCIDENCIA DE FRECUENCIAS ARMONICAS NATURALES DE VIBRACION DEL ALABE CON FRECUENCIAS DE ROTACION DE LA TURBINA, O CON SUS ARMONICOS. SE INCLUYEN MODIFICACIONES DE LA RAIZ DE LOS ALABES PARA FACILITAR SU INSTALACION.
ES9001190A 1989-04-27 1990-04-26 Alabe de extremidad de baja presion presion para un turbina de vapor de baja presion. Expired - Lifetime ES2024210A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/344,136 US4900230A (en) 1989-04-27 1989-04-27 Low pressure end blade for a low pressure steam turbine

Publications (1)

Publication Number Publication Date
ES2024210A6 true ES2024210A6 (es) 1992-02-16

Family

ID=23349219

Family Applications (1)

Application Number Title Priority Date Filing Date
ES9001190A Expired - Lifetime ES2024210A6 (es) 1989-04-27 1990-04-26 Alabe de extremidad de baja presion presion para un turbina de vapor de baja presion.

Country Status (7)

Country Link
US (1) US4900230A (es)
JP (1) JPH0361603A (es)
KR (1) KR0152986B1 (es)
CN (1) CN1046780A (es)
CA (1) CA2015562C (es)
ES (1) ES2024210A6 (es)
IT (1) IT1240290B (es)

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US5641268A (en) * 1991-09-17 1997-06-24 Rolls-Royce Plc Aerofoil members for gas turbine engines
US5203676A (en) * 1992-03-05 1993-04-20 Westinghouse Electric Corp. Ruggedized tapered twisted integral shroud blade
US5277549A (en) * 1992-03-16 1994-01-11 Westinghouse Electric Corp. Controlled reaction L-2R steam turbine blade
US5299915A (en) * 1992-07-15 1994-04-05 General Electric Corporation Bucket for the last stage of a steam turbine
US5286169A (en) * 1992-12-15 1994-02-15 General Electric Company Bucket for the next-to-last stage of a steam turbine
US5292230A (en) * 1992-12-16 1994-03-08 Westinghouse Electric Corp. Curvature steam turbine vane airfoil
US5267834A (en) * 1992-12-30 1993-12-07 General Electric Company Bucket for the last stage of a steam turbine
US5480285A (en) * 1993-08-23 1996-01-02 Westinghouse Electric Corporation Steam turbine blade
US5352092A (en) * 1993-11-24 1994-10-04 Westinghouse Electric Corporation Light weight steam turbine blade
US5524341A (en) * 1994-09-26 1996-06-11 Westinghouse Electric Corporation Method of making a row of mix-tuned turbomachine blades
CN1246570C (zh) * 1999-10-15 2006-03-22 株式会社日立制作所 透平动叶
US20060073022A1 (en) * 2004-10-05 2006-04-06 Gentile David P Frequency tailored thickness blade for a turbomachine wheel
JP4665916B2 (ja) * 2007-02-28 2011-04-06 株式会社日立製作所 ガスタービンの第１段動翼
US7988424B2 (en) * 2009-03-25 2011-08-02 General Electric Company Bucket for the last stage of a steam turbine
CN102444426B (zh) 2010-09-30 2015-05-27 阿尔斯通技术有限公司 改装汽轮机的方法
US8714930B2 (en) 2011-09-12 2014-05-06 General Electric Company Airfoil shape for turbine bucket and turbine incorporating same
US8845296B2 (en) 2011-09-19 2014-09-30 General Electric Company Airfoil shape for turbine bucket and turbine incorporating same
US8864457B2 (en) * 2011-10-06 2014-10-21 Siemens Energy, Inc. Gas turbine with optimized airfoil element angles
EP3985226B1 (en) 2014-02-19 2024-12-25 RTX Corporation Gas turbine engine airfoil
EP3108100B1 (en) 2014-02-19 2021-04-14 Raytheon Technologies Corporation Gas turbine engine fan blade
WO2015175044A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
US10570915B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
WO2015126941A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015175043A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
WO2015126448A1 (en) * 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
WO2015175052A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
EP3575551B1 (en) 2014-02-19 2021-10-27 Raytheon Technologies Corporation Gas turbine engine airfoil
US10584715B2 (en) 2014-02-19 2020-03-10 United Technologies Corporation Gas turbine engine airfoil
EP3108106B1 (en) 2014-02-19 2022-05-04 Raytheon Technologies Corporation Gas turbine engine airfoil
US10570916B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
US10465702B2 (en) 2014-02-19 2019-11-05 United Technologies Corporation Gas turbine engine airfoil
WO2015175073A2 (en) 2014-02-19 2015-11-19 United Technologies Corporation Gas turbine engine airfoil
EP3108120B1 (en) 2014-02-19 2021-03-31 Raytheon Technologies Corporation Gas turbine engine having a geared architecture and a specific fixed airfoil structure
US10495106B2 (en) 2014-02-19 2019-12-03 United Technologies Corporation Gas turbine engine airfoil
EP3108123B1 (en) 2014-02-19 2023-10-04 Raytheon Technologies Corporation Turbofan engine with geared architecture and lpc airfoils
EP3108103B1 (en) 2014-02-19 2023-09-27 Raytheon Technologies Corporation Fan blade for a gas turbine engine
EP3108105B1 (en) 2014-02-19 2021-05-12 Raytheon Technologies Corporation Gas turbine engine airfoil
US9567858B2 (en) 2014-02-19 2017-02-14 United Technologies Corporation Gas turbine engine airfoil
WO2015126454A1 (en) 2014-02-19 2015-08-27 United Technologies Corporation Gas turbine engine airfoil
EP3108101B1 (en) 2014-02-19 2022-04-20 Raytheon Technologies Corporation Gas turbine engine airfoil
US9140127B2 (en) 2014-02-19 2015-09-22 United Technologies Corporation Gas turbine engine airfoil
US11428241B2 (en) * 2016-04-22 2022-08-30 Raytheon Technologies Corporation System for an improved stator assembly
EP3361049A1 (de) * 2017-02-10 2018-08-15 Siemens Aktiengesellschaft Verfahren zum modifizieren einer turbine
US10408072B2 (en) * 2017-05-08 2019-09-10 General Electric Company Turbine nozzle airfoil profile
US10920594B2 (en) 2018-12-12 2021-02-16 Solar Turbines Incorporated Modal response tuned turbine blade
US11156092B2 (en) 2019-02-07 2021-10-26 Honeywell International Inc. Multistage axial-centrifugal compressor systems and methods for manufacture
CN109989792A (zh) * 2019-05-24 2019-07-09 哈尔滨汽轮机厂有限责任公司 全转速汽轮机末级动叶片

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US2258793A (en) * 1940-03-19 1941-10-14 Westinghouse Electric & Mfg Co Elastic-fluid turbine
US2934259A (en) * 1956-06-18 1960-04-26 United Aircraft Corp Compressor blading
FR1442526A (fr) * 1965-05-07 1966-06-17 Rateau Soc Perfectionnements aux canaux courbes parcourus par un gaz ou une vapeur
US3475108A (en) * 1968-02-14 1969-10-28 Siemens Ag Blade structure for turbines
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Also Published As

Publication number Publication date
IT1240290B (it) 1993-12-07
CN1046780A (zh) 1990-11-07
KR900016585A (ko) 1990-11-13
CA2015562C (en) 1999-12-28
JPH0361603A (ja) 1991-03-18
US4900230A (en) 1990-02-13
CA2015562A1 (en) 1990-10-27
IT9020013A1 (it) 1991-10-12
KR0152986B1 (ko) 1998-11-16
IT9020013A0 (it) 1990-04-12

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19980401