ES2052437A2 - Diseño de alabe perfeccionado con refuerzo integrante. - Google Patents

Diseño de alabe perfeccionado con refuerzo integrante.

Info

Publication number
ES2052437A2
ES2052437A2 ES09200575A ES9200575A ES2052437A2 ES 2052437 A2 ES2052437 A2 ES 2052437A2 ES 09200575 A ES09200575 A ES 09200575A ES 9200575 A ES9200575 A ES 9200575A ES 2052437 A2 ES2052437 A2 ES 2052437A2
Authority
ES
Spain
Prior art keywords
integral shroud
shroud
blade design
shroud blade
tip
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.)
Granted
Application number
ES09200575A
Other languages
English (en)
Other versions
ES2052437R (es
ES2052437B1 (es
Inventor
Jurek Ferleger
Harry Francis Martin
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 ES2052437A2 publication Critical patent/ES2052437A2/es
Publication of ES2052437R publication Critical patent/ES2052437R/es
Application granted granted Critical
Publication of ES2052437B1 publication Critical patent/ES2052437B1/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/24Blade-to-blade connections, e.g. for damping vibrations using wire or the like
    • 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
    • F01D5/16Form or construction for counteracting blade vibration
    • 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
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/50Vibration damping features
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making

Landscapes

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

Abstract

DISEÑO DE ALABE PERFECCIONADO CON REFUERZO INTEGRANTE QUE COMPRENDE UNA PARTE DE RAIZ PARA MONTAR EL ALABE EN UNA CORONA SOBRE UN ROTOR DE TURBINA; UNA PARTE DE PLATAFORMA; UNA PARTE DE HOJA AERODINAMICA EXTENDIDA HACIA ARRIBA DESDE LA PARTE DE PLATAFORMA Y QUE TIENE UN BORDE ANTERIOR, UN BORDE POSTERIOR Y UNA PUNTA; UN REFUERZO FORMADO EN LA PUNTA DE LA PARTE DE HOJA AERODINAMICA Y QUE TIENE DOS SUPERFICIES LATERALES TANGENCIALES OPUESTAS Y UNA SUPERFICIE SUPERIOR; Y AL MENOS UN PAR DE ORIFICIOS, ESTANDO FORMADO UN ORIFICIO DE CADA PAR EN CADA UNO DE LOS LADOS TANGENCIALES DEL REFUERZO.
ES09200575A 1991-03-28 1992-03-17 Diseño de alabe perfeccionado con refuerzo integrante. Expired - Lifetime ES2052437B1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/676,413 US5156529A (en) 1991-03-28 1991-03-28 Integral shroud blade design

Publications (3)

Publication Number Publication Date
ES2052437A2 true ES2052437A2 (es) 1994-07-01
ES2052437R ES2052437R (es) 1996-07-01
ES2052437B1 ES2052437B1 (es) 1997-02-16

Family

ID=24714405

Family Applications (1)

Application Number Title Priority Date Filing Date
ES09200575A Expired - Lifetime ES2052437B1 (es) 1991-03-28 1992-03-17 Diseño de alabe perfeccionado con refuerzo integrante.

Country Status (4)

Country Link
US (1) US5156529A (es)
JP (1) JPH0586804A (es)
CA (1) CA2064361A1 (es)
ES (1) ES2052437B1 (es)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5203676A (en) * 1992-03-05 1993-04-20 Westinghouse Electric Corp. Ruggedized tapered twisted integral shroud blade
US5365663A (en) * 1992-04-28 1994-11-22 Westinghouse Electric Corporation Method of attaching a monitor target to a shrouded blade
DE4324960A1 (de) * 1993-07-24 1995-01-26 Mtu Muenchen Gmbh Laufrad einer Turbomaschine, insbesondere einer Turbine eines Gasturbinentriebwerks
US5352092A (en) * 1993-11-24 1994-10-04 Westinghouse Electric Corporation Light weight steam turbine blade
US5522705A (en) * 1994-05-13 1996-06-04 United Technologies Corporation Friction damper for gas turbine engine blades
DE4432999C2 (de) * 1994-09-16 1998-07-30 Mtu Muenchen Gmbh Laufrad einer Turbomaschine, insbesondere einer axial durchströmten Turbine eines Gasturbinentriebwerks
US5667361A (en) * 1995-09-14 1997-09-16 United Technologies Corporation Flutter resistant blades, vanes and arrays thereof for a turbomachine
US6482533B2 (en) 2001-03-05 2002-11-19 The Boeing Company Article having imbedded cavity
JP4765882B2 (ja) * 2006-10-05 2011-09-07 株式会社日立製作所 蒸気タービン動翼
EP1985803A1 (de) * 2007-04-23 2008-10-29 Siemens Aktiengesellschaft Verfahren zum Herstellen von beschichteten Turbinenlaufschaufeln
US20100166550A1 (en) * 2008-12-31 2010-07-01 Devangada Siddaraja M Methods, systems and/or apparatus relating to frequency-tuned turbine blades
EP2221454A1 (en) * 2009-02-24 2010-08-25 Alstom Technology Ltd Gas turbine shrouded blade
ES2869338T3 (es) * 2011-10-07 2021-10-25 MTU Aero Engines AG Anillo de refuerzo de una paleta para una turbomaquinaria
US8894368B2 (en) 2012-01-04 2014-11-25 General Electric Company Device and method for aligning tip shrouds
ITTO20120517A1 (it) * 2012-06-14 2013-12-15 Avio Spa Schiera di profili aerodinamici per un impianto di turbina a gas
EP2938832B1 (en) * 2012-12-28 2019-02-06 United Technologies Corporation Shrouded turbine blade with cut corner
JP6779629B2 (ja) * 2016-02-04 2020-11-04 三菱パワー株式会社 動翼、回転機械及び動翼の振動数調整方法
KR101985103B1 (ko) * 2017-10-30 2019-05-31 두산중공업 주식회사 가스 터빈

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4097192A (en) * 1977-01-06 1978-06-27 Curtiss-Wright Corporation Turbine rotor and blade configuration
GB2106997A (en) * 1981-10-01 1983-04-20 Rolls Royce Vibration damped rotor blade for a turbomachine
US4441859A (en) * 1981-02-12 1984-04-10 Rolls-Royce Limited Rotor blade for a gas turbine engine
US4484859A (en) * 1980-01-17 1984-11-27 Rolls-Royce Limited Rotor blade for a gas turbine engine
US4767273A (en) * 1987-02-24 1988-08-30 Westinghouse Electric Corp. Apparatus and method for reducing blade flop in steam turbine
US4878810A (en) * 1988-05-20 1989-11-07 Westinghouse Electric Corp. Turbine blades having alternating resonant frequencies

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2430140A (en) * 1945-04-06 1947-11-04 Northrop Hendy Company Turbine blade and mounting
US3649133A (en) * 1970-09-10 1972-03-14 Westinghouse Electric Corp Rotor blade coupler arrangement
CH666722A5 (de) * 1985-07-05 1988-08-15 Bbc Brown Boveri & Cie Laufschaufelkranz einer axial durchstroemten turbomaschine.
US4776764A (en) * 1987-04-02 1988-10-11 Ortolano Ralph J Structure for an axial flow elastic fluid utilizing machine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4097192A (en) * 1977-01-06 1978-06-27 Curtiss-Wright Corporation Turbine rotor and blade configuration
US4484859A (en) * 1980-01-17 1984-11-27 Rolls-Royce Limited Rotor blade for a gas turbine engine
US4441859A (en) * 1981-02-12 1984-04-10 Rolls-Royce Limited Rotor blade for a gas turbine engine
GB2106997A (en) * 1981-10-01 1983-04-20 Rolls Royce Vibration damped rotor blade for a turbomachine
US4767273A (en) * 1987-02-24 1988-08-30 Westinghouse Electric Corp. Apparatus and method for reducing blade flop in steam turbine
US4878810A (en) * 1988-05-20 1989-11-07 Westinghouse Electric Corp. Turbine blades having alternating resonant frequencies

Also Published As

Publication number Publication date
CA2064361A1 (en) 1992-09-29
ES2052437R (es) 1996-07-01
ES2052437B1 (es) 1997-02-16
JPH0586804A (ja) 1993-04-06
US5156529A (en) 1992-10-20

Similar Documents

Publication Publication Date Title
ES2052437A2 (es) Diseño de alabe perfeccionado con refuerzo integrante.
ES2024761A6 (es) Montaje de alabes de turbina de plataforma integral con raices de entrada lateral oblicua.
SE8503614D0 (sv) Gas turbine bladed disk assembly
CA2130628A1 (en) Steam turbine blade
EP0887513A3 (en) Turbine blade
EP1122405A3 (en) Gas turbine bucket cooling circuit
ATE174664T1 (de) Wurzelprofil für windturbine
ATE335917T1 (de) Turbomaschinenschaufel mit versetzter spitzenkante
EP0916811A3 (en) Ribbed turbine blade tip
CA2070099A1 (en) Freestanding mixed tuned steam turbine blade
ATE483098T1 (de) Gasturbinenschaufel mit prallgekühlter plattform
CA2327857A1 (en) Turbine nozzle with sloped film cooling
WO1998051457A3 (en) Razor assembly
KR910008254A (ko) 반동 터어빈 블레이드 열 용 블레이드
MXPA02008461A (es) Helice de alto rendimiento.
CA2254230A1 (en) Gas turbine rotor blade
CA2196481A1 (en) Steam Turbine
EP0924380A3 (en) Striated turbomachine blade
GB1500858A (en) Blade for thermal axial-flow turbo machines
EP0250062A3 (en) Propeller blade
DK1163832T3 (da) Skæremaskine
KR880014231A (ko) 터어빈 블레이드의 장착방법
GB2105415B (en) Air-cooled turbine rotor blade with trailing edge recessed holes
WO1994012390A3 (en) Coolable rotor blade structure
IT8941506A0 (it) Supporto di palette e complesso di palette in particolare per turbine a fluidi.

Legal Events

Date Code Title Description
EC2A Search report published

Date of ref document: 19920317

Kind code of ref document: B1

Effective date: 19920317

FA2A Application withdrawn

Effective date: 19980324