BE829439A - Turbomachine munie d'un dispositif d'equilibrage - Google Patents

Turbomachine munie d'un dispositif d'equilibrage

Info

Publication number
BE829439A
BE829439A BE156667A BE156667A BE829439A BE 829439 A BE829439 A BE 829439A BE 156667 A BE156667 A BE 156667A BE 156667 A BE156667 A BE 156667A BE 829439 A BE829439 A BE 829439A
Authority
BE
Belgium
Prior art keywords
balancing device
turbomachine equipped
turbomachine
balancing
Prior art date
Application number
BE156667A
Other languages
English (en)
French (fr)
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 filed Critical
Publication of BE829439A publication Critical patent/BE829439A/xx

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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/027—Arrangements for balancing
    • 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
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE156667A 1974-05-23 1975-05-23 Turbomachine munie d'un dispositif d'equilibrage BE829439A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US472815A US3888601A (en) 1974-05-23 1974-05-23 Turbomachine with balancing means

Publications (1)

Publication Number Publication Date
BE829439A true BE829439A (fr) 1975-09-15

Family

ID=23877047

Family Applications (1)

Application Number Title Priority Date Filing Date
BE156667A BE829439A (fr) 1974-05-23 1975-05-23 Turbomachine munie d'un dispositif d'equilibrage

Country Status (7)

Country Link
US (1) US3888601A (de)
JP (1) JPS50150908A (de)
BE (1) BE829439A (de)
DE (1) DE2514947A1 (de)
FR (1) FR2272260B1 (de)
GB (1) GB1500575A (de)
IT (1) IT1037742B (de)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4033705A (en) * 1976-04-26 1977-07-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Blade retainer assembly
FR2404212A1 (fr) * 1977-09-23 1979-04-20 Snecma Dispositif d'equilibrage d'un rotor
US4275990A (en) * 1977-12-17 1981-06-30 Rolls-Royce Limited Disc channel for cooling rotor blade roots
US4221542A (en) * 1977-12-27 1980-09-09 General Electric Company Segmented blade retainer
GB2054058B (en) * 1979-06-16 1983-04-20 Rolls Royce Reducing rotor noise
US4344740A (en) * 1979-09-28 1982-08-17 United Technologies Corporation Rotor assembly
US4347040A (en) * 1980-10-02 1982-08-31 United Technologies Corporation Blade to blade vibration damper
USRE32339E (en) * 1980-10-02 1987-01-27 United Technologies Corporation Blade to blade vibration damper
FR2499652A1 (fr) * 1981-02-11 1982-08-13 Snecma Dispositif de correction de balourd de rotor de turbomachines
US4355957A (en) * 1981-06-18 1982-10-26 United Technologies Corporation Blade damper
US4477226A (en) * 1983-05-09 1984-10-16 General Electric Company Balance for rotating member
US4848182A (en) * 1987-09-08 1989-07-18 United Technologies Corporation Rotor balance system
US4926710A (en) * 1987-09-08 1990-05-22 United Technologies Corporation Method of balancing bladed gas turbine engine rotor
US4803893A (en) * 1987-09-24 1989-02-14 United Technologies Corporation High speed rotor balance system
US4898514A (en) * 1987-10-27 1990-02-06 United Technologies Corporation Turbine balance arrangement with integral air passage
FR2639402B1 (fr) * 1988-11-23 1990-12-28 Snecma Disque ailete de rotor de turbomachine
US4890981A (en) * 1988-12-30 1990-01-02 General Electric Company Boltless rotor blade retainer
US5018943A (en) * 1989-04-17 1991-05-28 General Electric Company Boltless balance weight for turbine rotors
GB2250783B (en) * 1990-11-03 1995-01-04 Papst Motoren Gmbh & Co Kg Improvements in or relating to fan impellers
US5151013A (en) * 1990-12-27 1992-09-29 United Technologies Corporation Blade lock for a rotor disk and rotor blade assembly
GB9302064D0 (en) * 1993-02-03 1993-03-24 Rolls Royce Plc Balanced rotor
US5350279A (en) * 1993-07-02 1994-09-27 General Electric Company Gas turbine engine blade retainer sub-assembly
FR2716931B1 (fr) * 1994-03-03 1996-04-05 Snecma Système d'équilibrage et d'amortissement d'un dique de turbomachine.
US6494679B1 (en) * 1999-08-05 2002-12-17 General Electric Company Apparatus and method for rotor damping
US6390777B1 (en) 1999-09-01 2002-05-21 Angelo Fan Brace Licensing, L.L.C. Quick-connect fan blade mounting assembly
US6951448B2 (en) * 2002-04-16 2005-10-04 United Technologies Corporation Axial retention system and components thereof for a bladed rotor
US6908285B2 (en) * 2003-04-08 2005-06-21 General Electric Company Methods and apparatus for assembling rotatable machines
US6976827B2 (en) * 2003-10-14 2005-12-20 Pratt & Whitney Canada Corp. Rotor balancing device and method
FR2866057B1 (fr) * 2004-02-06 2006-04-28 Snecma Moteurs Dispositif d'equilibrage d'un disque de rotor, disque equipe d'un tel dispositif, et rotor ayant un tel disque
US7287958B2 (en) * 2005-01-10 2007-10-30 General Electric Company Methods and apparatus for assembling rotatable machines
US7530791B2 (en) * 2005-12-22 2009-05-12 Pratt & Whitney Canada Corp. Turbine blade retaining apparatus
JP2007247406A (ja) * 2006-03-13 2007-09-27 Ihi Corp ファンブレードの保持構造
FR2918106B1 (fr) * 2007-06-27 2011-05-06 Snecma Dispositif de retenue axiale d'aubes montees sur un disque de rotor de turbomachine.
DE102007059220A1 (de) * 2007-12-07 2009-06-10 Rolls-Royce Deutschland Ltd & Co Kg Leitschaufelkranz für thermische Strömungsmaschinen, insbesondere Flugtriebwerke
FR2939832B1 (fr) * 2008-12-11 2011-01-07 Turbomeca Roue de turbine equipee d'un dispositif de retenue axiale verrouillant des pales par rapport a un disque.
FR2951224B1 (fr) * 2009-10-13 2011-12-09 Turbomeca Roue de turbine equipee d'un jonc de retenue axiale verrouillant des pales par rapport a un disque
RU2516722C1 (ru) * 2012-11-15 2014-05-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Ротор с компенсатором дисбаланса
US9404367B2 (en) * 2012-11-21 2016-08-02 Solar Turbines Incorporated Gas turbine engine compressor rotor assembly and balancing system
FR3000763B1 (fr) * 2013-01-04 2016-07-15 Snecma Disque de rotor muni d’une pluralite de crochets
EP3006667A1 (de) * 2014-10-09 2016-04-13 Siemens Aktiengesellschaft Turbinenlaufschaufel, Anordnung aus einer Turbinenwelle, einer Turbinenradscheibe, einer Vielzahl an Turbinenlaufschaufeln sowie einem Wuchtgewicht und Turbine
US10436224B2 (en) 2016-04-01 2019-10-08 General Electric Company Method and apparatus for balancing a rotor
US10883370B2 (en) * 2018-08-14 2021-01-05 Raytheon Technologies Corporation Dovetail weight system for rotor balance
CN112160794B (zh) * 2020-09-18 2023-02-17 中国航发四川燃气涡轮研究院 定位组件及其涡轮盘或压气机盘、航空发动机
RU209925U1 (ru) * 2021-12-27 2022-03-23 Публичное Акционерное Общество "Одк-Сатурн" Узел ротора турбины большой мощности

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836392A (en) * 1953-06-03 1958-05-27 United Aircraft Corp Disc vibration damping means
US2957675A (en) * 1956-05-07 1960-10-25 Gen Electric Damping means
US2999668A (en) * 1958-08-28 1961-09-12 Curtiss Wright Corp Self-balanced rotor blade
US3034764A (en) * 1959-12-18 1962-05-15 Gen Electric Damping means
US3129921A (en) * 1962-07-06 1964-04-21 United Aircraft Corp Blade damping device
US3181835A (en) * 1964-01-07 1965-05-04 Carroll C Davis Blade vibration damping device
US3341174A (en) * 1967-02-27 1967-09-12 United Aircraft Corp Blade lock

Also Published As

Publication number Publication date
DE2514947A1 (de) 1975-12-11
GB1500575A (en) 1978-02-08
FR2272260A1 (de) 1975-12-19
FR2272260B1 (de) 1979-03-30
IT1037742B (it) 1979-11-20
US3888601A (en) 1975-06-10
JPS50150908A (de) 1975-12-04

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