ES2007867A6 - Metodo para instalar alabes de turbina con refuerzo enterizo. - Google Patents

Metodo para instalar alabes de turbina con refuerzo enterizo.

Info

Publication number
ES2007867A6
ES2007867A6 ES8801577A ES8801577A ES2007867A6 ES 2007867 A6 ES2007867 A6 ES 2007867A6 ES 8801577 A ES8801577 A ES 8801577A ES 8801577 A ES8801577 A ES 8801577A ES 2007867 A6 ES2007867 A6 ES 2007867A6
Authority
ES
Spain
Prior art keywords
blades
blade
anchor
rotor
integral shroud
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
ES8801577A
Other languages
English (en)
Inventor
Albert Joseph Partington
David Allen Hornberger
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.)
CBS 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 ES2007867A6 publication Critical patent/ES2007867A6/es
Expired 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/16—Joints and connections with adjunctive protector, broken parts retainer, repair, assembly or disassembly feature
    • Y10T403/1608—Holding means or protector functioning only during transportation, assembly or disassembly

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

EN UN METODO PARA INSTALAR UN GRUPO O CONJUNTO DE ALABES DE TURBINA GIRATORIOS, CADA UNO DE LOS CUALES TIENE UN SEGMENTO DE REFUERZO ENTERIZO, SE INSTALA UN ANCLAJE DE ALABE RETIRABLE PARA INSTALAR LOS ALABES DE TURBINA, DESPUES DE LO CUAL, SE ACUÑA UNA PLURALIDAD DE ALABES IN SITU ALREDEDOR DEL ROTOR, DE MODO QUE EL SEGMENTO DE REFUERZO ENTERIZO DE CADA ALABE HAGA TOPE CON UN SEGMENTO DE REFUERZO ENTERIZO ADYACENTE Y TODOS LOS SEGMENTOS DE REFUERZO ENTERIZO ADYACENTE Y TODOS LOS SEGMENTOS DE REFUERZO SON FORZADOS CONTRA EL ANCLAJE DEL ALABE. A CONTINUACION, UNA PRIMERA PARTE O PORCION DE LOS ALABES SON ACUÑADOS DE NUEVO A FIN DE FORZAR A LA PRIMERA PARTE DE ALABES FUERA DEL ANCLAJE DE ALABES. EL ANCLAJE DE ALABES ES A CONTINUACION RETIRADO SIN PERTURBAR AL INTIMO CONTACTO ENTRE LA PLURALIDAD DE ALABES Y SE INSTALAN ALABES ADICIONALES PARA COMPLETAR LA HILERA DE ALABES.
ES8801577A 1987-05-22 1988-05-19 Metodo para instalar alabes de turbina con refuerzo enterizo. Expired ES2007867A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/053,246 US4798520A (en) 1987-05-22 1987-05-22 Method for installing integral shroud turbine blading

Publications (1)

Publication Number Publication Date
ES2007867A6 true ES2007867A6 (es) 1989-07-01

Family

ID=21982881

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8801577A Expired ES2007867A6 (es) 1987-05-22 1988-05-19 Metodo para instalar alabes de turbina con refuerzo enterizo.

Country Status (7)

Country Link
US (1) US4798520A (es)
JP (1) JPS63306207A (es)
KR (1) KR880014230A (es)
CN (1) CN1012912B (es)
CA (1) CA1319500C (es)
ES (1) ES2007867A6 (es)
IT (1) IT1220702B (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5001830A (en) * 1989-10-23 1991-03-26 Westinghouse Electric Corp. Method for assembling side entry control stage blades in a steam turbine
US5174715A (en) * 1990-12-13 1992-12-29 General Electric Company Turbine nozzle
US5182855A (en) * 1990-12-13 1993-02-02 General Electric Company Turbine nozzle manufacturing method
JP3034417B2 (ja) * 1994-02-18 2000-04-17 株式会社東芝 軸流タービンの動翼制振装置
CN100338337C (zh) * 2002-06-07 2007-09-19 三菱重工业株式会社 汽轮机转子叶片组件及其组装方法
US7284958B2 (en) * 2003-03-22 2007-10-23 Allison Advanced Development Company Separable blade platform
KR100642466B1 (ko) * 2005-10-07 2006-11-02 두산중공업 주식회사 터빈용 로터의 일체형 버킷조립용 지그
CN100494563C (zh) * 2006-05-30 2009-06-03 王心伯 高档漂白棉浆板的制浆方法
US7975354B2 (en) * 2007-02-08 2011-07-12 United Technologies Corporation Bladed disk assembly method and impact device
US7971334B2 (en) * 2008-01-22 2011-07-05 United Technologies Corporation Bladed disk assembly method and roller device
US8894368B2 (en) * 2012-01-04 2014-11-25 General Electric Company Device and method for aligning tip shrouds

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB751740A (en) * 1953-10-02 1956-07-04 English Electric Co Ltd Improvements in and relating to the fixing of rotor blades of axial flow turbines and compressors
US3158353A (en) * 1962-07-16 1964-11-24 United Aircraft Canada Blade locking device for conical broached discs
US3627448A (en) * 1969-12-31 1971-12-14 Westinghouse Electric Corp Locking arrangement for side-entry blades
US4451205A (en) * 1982-02-22 1984-05-29 United Technologies Corporation Rotor blade assembly

Also Published As

Publication number Publication date
CN1012912B (zh) 1991-06-19
US4798520A (en) 1989-01-17
CA1319500C (en) 1993-06-29
IT8841607A0 (it) 1988-05-20
CN88103006A (zh) 1988-12-21
IT1220702B (it) 1990-06-15
KR880014230A (ko) 1988-12-23
JPS63306207A (ja) 1988-12-14
JPH0579801B2 (es) 1993-11-04

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19980504