ES2087775T3 - Dispositivo para la proteccion axial de alabes de rodete y para la eliminacion de los desequilibrios del rotor para compresores o turbinas de circulacion axial. - Google Patents

Dispositivo para la proteccion axial de alabes de rodete y para la eliminacion de los desequilibrios del rotor para compresores o turbinas de circulacion axial.

Info

Publication number
ES2087775T3
ES2087775T3 ES94100329T ES94100329T ES2087775T3 ES 2087775 T3 ES2087775 T3 ES 2087775T3 ES 94100329 T ES94100329 T ES 94100329T ES 94100329 T ES94100329 T ES 94100329T ES 2087775 T3 ES2087775 T3 ES 2087775T3
Authority
ES
Spain
Prior art keywords
axial
base
rotor
cavity
elimination
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
ES94100329T
Other languages
English (en)
Inventor
Karl Maar
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Application granted granted Critical
Publication of ES2087775T3 publication Critical patent/ES2087775T3/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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • F01D5/323—Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/662—Balancing of rotors
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/30—Compensating imbalance
    • G01M1/32—Compensating imbalance by adding material to the body to be tested, e.g. by correcting-weights

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

SE INDICA UN DISPOSITIVO PARA LA SEGURIDAD DE FUNCIONAMIENTO AXIAL DEL ALABE Y PARA LA ELIMINACION DE LA DESCOMPENSACION DEL ROTOR PARA EL COMPRESOR AXIAL O TURBINAS DE MOTOPROPULSORES DE TURBINAS DE GAS, EN EL QUE LOS ALABES (1) DE FUNCIONAMIENTO CON SUS BASES (2) SE ANCLAN EN RANURAS (3) AXIALES DEL DISCO (4) DE LA RUEDA DISTRIBUIDOS POR LA PERIFERIA; POR LO QUE CADA RANURA AXIAL INCLUYE UNA CAVIDAD (T) FORMADA ENTRE LA BASE DE LA RANURA Y EL EXTREMO DE LA BASE; EN CADA CAVIDAD SE COLOCA UNA PIEZA (5) DE RELLENO INSTALADA SOBRE LA BASE DE LA RANURA Y UNA CHAPA (6) DE SEGURIDAD QUE PUENTEA ENTRE EL EXTREMO DE LA BASE Y LA PIEZA DE RELLENO UNA GRIETA (S) QUE PASA A LO LARGO DE LA CAVIDAD, QUE SE DOBLA EN AMBOS EXTREMOS ALINEADOS DE FORMA OPUESTA Y QUE SOBRESALEN DE LA CAVIDAD FRENTE A LA SUPERFICIE FRONTAL, EL DISCO DE RUEDA Y LA BASE DEL ALABE, POR LO QUE UNA DESCOMPENSACION DEL ROTOR SE COMPENSA EN PESO A TRAVES DE UNA PIEZA DE RELLENO.
ES94100329T 1993-01-14 1994-01-12 Dispositivo para la proteccion axial de alabes de rodete y para la eliminacion de los desequilibrios del rotor para compresores o turbinas de circulacion axial. Expired - Lifetime ES2087775T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4300773A DE4300773C1 (de) 1993-01-14 1993-01-14 Einrichtung zur axialen Laufschaufelsicherung und zur Beseitigung von Rotorunwuchten für axial durchströmte Verdichter oder Turbinen

Publications (1)

Publication Number Publication Date
ES2087775T3 true ES2087775T3 (es) 1996-07-16

Family

ID=6478161

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94100329T Expired - Lifetime ES2087775T3 (es) 1993-01-14 1994-01-12 Dispositivo para la proteccion axial de alabes de rodete y para la eliminacion de los desequilibrios del rotor para compresores o turbinas de circulacion axial.

Country Status (6)

Country Link
US (1) US5425621A (es)
EP (1) EP0610668B1 (es)
JP (1) JP3081098B2 (es)
CA (1) CA2113376C (es)
DE (1) DE4300773C1 (es)
ES (1) ES2087775T3 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4430636C2 (de) * 1994-08-29 1997-01-23 Mtu Muenchen Gmbh Einrichtung zur Laufschaufelfixierung und zur Beseitigung von Rotorunwuchten bei axial durchströmten Verdichtern oder Turbinen von Gasturbinentriebwerken
US5720596A (en) * 1997-01-03 1998-02-24 Westinghouse Electric Corporation Apparatus and method for locking blades into a rotor
RU2146767C1 (ru) * 1998-02-23 2000-03-20 Открытое акционерное общество "Авиадвигатель" Рабочее колесо турбомашины
FR2807096B1 (fr) * 2000-03-30 2002-05-31 Abb Alstom Power Nv Disque rotorique de turbine equipe d'ailettes a pied de sapin et procede de montage d'une ailette sur un disque
DE102005024932A1 (de) 2005-05-31 2006-12-07 Rolls-Royce Deutschland Ltd & Co Kg Turbinenschaufelaxialsperre
DE502007001344D1 (de) * 2007-01-09 2009-10-01 Siemens Ag Biegevorrichtung zum Einbiegen eines Sicherungsbleches eines Rotors einer Turbine
EP2455588B1 (de) 2010-11-15 2017-03-01 MTU Aero Engines GmbH Sicherungsmittel zur axialen Sicherung eines Schaufelfußes einer Turbomaschinenschaufel
GB2491121B (en) * 2011-05-23 2014-10-01 Rolls Royce Plc Balancing of rotatable components
EP2789800B1 (de) 2013-04-09 2017-06-14 MTU Aero Engines AG Sicherungsblechsortiment, zugehörige Gasturbine und Montageverfahren
PL2808486T3 (pl) * 2013-05-27 2017-11-30 MTU Aero Engines AG Element wyważający do układu łopatek wirujących
FR3008131B1 (fr) 2013-07-02 2016-09-30 Snecma Etage de turbine ou de compresseur comprenant une piece d'interface en materiau ceramique
US11339674B2 (en) 2018-08-14 2022-05-24 Rolls-Royce North American Technologies Inc. Blade retainer for gas turbine engine
DE102019206432A1 (de) * 2019-05-06 2020-11-12 MTU Aero Engines AG Turbomaschinenschaufel
US11555407B2 (en) * 2020-05-19 2023-01-17 General Electric Company Turbomachine rotor assembly

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB672401A (en) * 1950-03-25 1952-05-21 Armstrong Siddeley Motors Ltd Securing blades to a rotor
GB691380A (en) * 1950-07-01 1953-05-13 Power Jets Res & Dev Ltd Improvements relating to bladed rotors for compressors, turbines or like apparatus
BE537113A (es) * 1954-04-05
GB793930A (en) * 1954-08-10 1958-04-23 Joseph Thompson Purvis Rotor for rotary power conversion machines
US2828942A (en) * 1955-08-01 1958-04-01 Orenda Engines Ltd Rotor blade and rotor blade assembly
DE1051286B (de) * 1958-06-02 1959-02-26 Her Majesty The Queen In The R Sicherung fuer eine in einer Axialnut einer Kreiselmaschine gehaltene Schaufel
US3076634A (en) * 1959-06-12 1963-02-05 Ass Elect Ind Locking means for compressor and turbine blades
US3653781A (en) * 1970-12-18 1972-04-04 Gen Electric Turbomachinery blade retainer
DE2639200A1 (de) * 1976-08-31 1978-03-09 Volkswagenwerk Ag Laufrad fuer axialturbinen, insbesondere fuer gasturbinen
GB2105790A (en) * 1981-09-15 1983-03-30 Rolls Royce Balanced bladed rotor
US4477226A (en) * 1983-05-09 1984-10-16 General Electric Company Balance for rotating member
US4898514A (en) * 1987-10-27 1990-02-06 United Technologies Corporation Turbine balance arrangement with integral air passage
EP0437977A1 (en) * 1990-01-18 1991-07-24 United Technologies Corporation Turbine rim configuration

Also Published As

Publication number Publication date
CA2113376A1 (en) 1994-07-15
US5425621A (en) 1995-06-20
DE4300773C1 (de) 1993-11-18
CA2113376C (en) 2005-04-26
EP0610668A1 (de) 1994-08-17
JP3081098B2 (ja) 2000-08-28
JPH0754605A (ja) 1995-02-28
EP0610668B1 (de) 1996-05-01

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