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ES441838A1 - Un rotor perfeccionado para un aparato de turbina de vapor con flujo axial y un metodo para sustituir un alabe en dichoaparato. - Google Patents

Un rotor perfeccionado para un aparato de turbina de vapor con flujo axial y un metodo para sustituir un alabe en dichoaparato.

Info

Publication number
ES441838A1
ES441838A1 ES441838A ES441838A ES441838A1 ES 441838 A1 ES441838 A1 ES 441838A1 ES 441838 A ES441838 A ES 441838A ES 441838 A ES441838 A ES 441838A ES 441838 A1 ES441838 A1 ES 441838A1
Authority
ES
Spain
Prior art keywords
arched
curvature
radius
shape
rotor
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
ES441838A
Other languages
English (en)
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 ES441838A1 publication Critical patent/ES441838A1/es
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32Locking, e.g. by final locking blades or keys
    • F01D5/326Locking of axial insertion type blades by other means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00Restoring or reconditioning objects
    • B23P6/002Repairing turbine components, e.g. moving or stationary blades, rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
ES441838A 1974-10-29 1975-10-16 Un rotor perfeccionado para un aparato de turbina de vapor con flujo axial y un metodo para sustituir un alabe en dichoaparato. Expired ES441838A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/518,909 US3986793A (en) 1974-10-29 1974-10-29 Turbine rotating blade

Publications (1)

Publication Number Publication Date
ES441838A1 true ES441838A1 (es) 1977-06-16

Family

ID=24065990

Family Applications (1)

Application Number Title Priority Date Filing Date
ES441838A Expired ES441838A1 (es) 1974-10-29 1975-10-16 Un rotor perfeccionado para un aparato de turbina de vapor con flujo axial y un metodo para sustituir un alabe en dichoaparato.

Country Status (12)

Country Link
US (1) US3986793A (es)
JP (1) JPS521202A (es)
BE (1) BE834920A (es)
CA (1) CA1034871A (es)
CH (1) CH601646A5 (es)
DE (1) DE2544952A1 (es)
ES (1) ES441838A1 (es)
FR (1) FR2289727A1 (es)
GB (1) GB1482308A (es)
IT (1) IT1043690B (es)
NL (1) NL7510469A (es)
SE (1) SE410487B (es)

Families Citing this family (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1513338A (en) * 1976-03-26 1978-06-07 Rolls Royce Rotor blade for a gas turbine engine
US4621979A (en) * 1979-11-30 1986-11-11 United Technologies Corporation Fan rotor blades of turbofan engines
US4767275A (en) * 1986-07-11 1988-08-30 Westinghouse Electric Corp. Locking pin system for turbine curved root side entry closing blades
US5001830A (en) * 1989-10-23 1991-03-26 Westinghouse Electric Corp. Method for assembling side entry control stage blades in a steam turbine
US5017091A (en) * 1990-02-26 1991-05-21 Westinghouse Electric Corp. Free standing blade for use in low pressure steam turbine
US5067876A (en) * 1990-03-29 1991-11-26 General Electric Company Gas turbine bladed disk
US5236309A (en) * 1991-04-29 1993-08-17 Westinghouse Electric Corp. Turbine blade assembly
US5160242A (en) * 1991-05-31 1992-11-03 Westinghouse Electric Corp. Freestanding mixed tuned steam turbine blade
US5286168A (en) * 1992-01-31 1994-02-15 Westinghouse Electric Corp. Freestanding mixed tuned blade
US5310318A (en) * 1993-07-21 1994-05-10 General Electric Company Asymmetric axial dovetail and rotor disk
FR2725239B1 (fr) 1994-09-30 1996-11-22 Gec Alsthom Electromec Disposition pour l'ecretement des pointes de contrainte dans l'ancrage d'une ailette de turbine, comportant une racine dite en "pied-sapin"
FR2743845B1 (fr) * 1996-01-23 1998-02-20 Snecma Aube mobile de soufflante a profil de securite
GB9615826D0 (en) * 1996-07-27 1996-09-11 Rolls Royce Plc Gas turbine engine fan blade retention
GB2345943B (en) * 1998-12-04 2003-07-09 Glenn Bruce Sinclair Precision crowning of blade attachments in gas turbines
US6371725B1 (en) * 2000-06-30 2002-04-16 General Electric Company Conforming platform guide vane
KR20020016093A (ko) * 2000-08-24 2002-03-04 이중구 가스터어빈엔진용 디스크
US6481971B1 (en) * 2000-11-27 2002-11-19 General Electric Company Blade spacer
US6457942B1 (en) * 2000-11-27 2002-10-01 General Electric Company Fan blade retainer
FR2856728B1 (fr) * 2003-06-27 2005-10-28 Snecma Moteurs Aube de compresseur de turboreacteur
US7261518B2 (en) * 2005-03-24 2007-08-28 Siemens Demag Delaval Turbomachinery, Inc. Locking arrangement for radial entry turbine blades
US7467922B2 (en) * 2005-07-25 2008-12-23 Siemens Aktiengesellschaft Cooled turbine blade or vane for a gas turbine, and use of a turbine blade or vane of this type
US7300253B2 (en) * 2005-07-25 2007-11-27 Siemens Aktiengesellschaft Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring
GB0521242D0 (en) * 2005-10-19 2005-11-23 Rolls Royce Plc A blade mounting
US7581924B2 (en) * 2006-07-27 2009-09-01 Siemens Energy, Inc. Turbine vanes with airfoil-proximate cooling seam
US7488157B2 (en) * 2006-07-27 2009-02-10 Siemens Energy, Inc. Turbine vane with removable platform inserts
EP1898049B1 (en) * 2006-09-11 2012-05-23 Siemens Aktiengesellschaft Turbine blade
US20080298973A1 (en) * 2007-05-29 2008-12-04 Siemens Power Generation, Inc. Turbine vane with divided turbine vane platform
US8459956B2 (en) * 2008-12-24 2013-06-11 General Electric Company Curved platform turbine blade
US20100166562A1 (en) * 2008-12-30 2010-07-01 General Electric Company Turbine blade root configurations
US20100166561A1 (en) * 2008-12-30 2010-07-01 General Electric Company Turbine blade root configurations
GB2470404B (en) 2009-05-22 2014-03-19 Phillips Screw Co Low energy screws for wood and similar materials
US8439643B2 (en) * 2009-08-20 2013-05-14 General Electric Company Biformal platform turbine blade
DE102010004854A1 (de) 2010-01-16 2011-07-21 MTU Aero Engines GmbH, 80995 Laufschaufel für eine Strömungsmaschine und Strömungsmaschine
US9033669B2 (en) * 2012-06-15 2015-05-19 General Electric Company Rotating airfoil component with platform having a recessed surface region therein
WO2014163680A1 (en) 2013-03-10 2014-10-09 Rivers Jonathan M Attachment feature of a gas turbine engine blade having a curved profile
JP6395498B2 (ja) * 2014-08-12 2018-09-26 三菱重工コンプレッサ株式会社 タービンロータディスクの翼溝部の超音波探傷方法及び装置
US10683765B2 (en) * 2017-02-14 2020-06-16 General Electric Company Turbine blades having shank features and methods of fabricating the same
US10895160B1 (en) 2017-04-07 2021-01-19 Glenn B. Sinclair Stress relief via unblended edge radii in blade attachments in gas turbines
US10584600B2 (en) * 2017-06-14 2020-03-10 General Electric Company Ceramic matrix composite (CMC) blade and method of making a CMC blade
CN109048220B (zh) * 2018-08-31 2021-03-23 中国航发贵州黎阳航空动力有限公司 一种更换飞机发动机叶片的方法
FR3085992B1 (fr) * 2018-09-14 2020-12-11 Safran Aircraft Engines Aube de roue mobile de turbine comportant un pied de forme curviligne
DE102020216436A1 (de) 2020-12-21 2022-06-23 MTU Aero Engines AG Rotorscheibe und Laufschaufel für eine Flugtriebwerk-Gasturbinen-Verdichter- oder Turbinenstufe

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US417865A (en) * 1889-12-24 Water-wheel
US1793468A (en) * 1929-05-28 1931-02-24 Westinghouse Electric & Mfg Co Turbine blade
US1719415A (en) * 1927-09-14 1929-07-02 Westinghouse Electric & Mfg Co Turbine-blade attachment
NL27859C (es) * 1928-12-29
DE767990C (de) * 1940-10-16 1955-05-05 Messerschmitt Boelkow Blohm Axial beaufschlagte Hohlschaufel fuer Kreiselmaschinen
GB725461A (en) * 1953-04-10 1955-03-02 Parsons C A & Co Ltd Improvements in and relating to the axial locking of rotor blades for turbines and the like
US2994507A (en) * 1959-01-23 1961-08-01 Westinghouse Electric Corp Blade locking structure
US3378230A (en) * 1966-12-16 1968-04-16 Gen Electric Mounting of blades in turbomachine rotors
US3490132A (en) * 1967-06-28 1970-01-20 Rodney D Kosters Method and apparatus for replacing timing gears
DE2140816A1 (de) * 1971-08-14 1973-03-01 Motoren Turbinen Union Rotor fuer stroemungsmaschinen
US3802046A (en) * 1972-01-27 1974-04-09 Chromalloy American Corp Method of making or reconditioning a turbine-nozzle or the like assembly
JPH085270Y2 (ja) * 1991-04-26 1996-02-14 三協アルミニウム工業株式会社 面格子付きサッシ

Also Published As

Publication number Publication date
JPS5410043B2 (es) 1979-05-01
FR2289727B1 (es) 1978-04-07
NL7510469A (nl) 1976-05-04
JPS521202A (en) 1977-01-07
GB1482308A (en) 1977-08-10
FR2289727A1 (fr) 1976-05-28
SE410487B (sv) 1979-10-15
BE834920A (fr) 1976-04-28
DE2544952A1 (de) 1976-05-06
SE7512117L (sv) 1976-04-30
CA1034871A (en) 1978-07-18
IT1043690B (it) 1980-02-29
CH601646A5 (es) 1978-07-14
US3986793A (en) 1976-10-19

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19971103