FR3108360B1 - Procede et dispositif d’equilibrage d’une piece tournante pour une turbomachine d’aeronef - Google Patents

Procede et dispositif d’equilibrage d’une piece tournante pour une turbomachine d’aeronef Download PDF

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Publication number
FR3108360B1
FR3108360B1 FR2002794A FR2002794A FR3108360B1 FR 3108360 B1 FR3108360 B1 FR 3108360B1 FR 2002794 A FR2002794 A FR 2002794A FR 2002794 A FR2002794 A FR 2002794A FR 3108360 B1 FR3108360 B1 FR 3108360B1
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FR
France
Prior art keywords
rotating part
balancing
aircraft turbomachine
rotation
axis
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.)
Active
Application number
FR2002794A
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English (en)
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FR3108360A1 (fr
Inventor
Guillaume Maurice René Patin
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.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
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.)
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Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR2002794A priority Critical patent/FR3108360B1/fr
Publication of FR3108360A1 publication Critical patent/FR3108360A1/fr
Application granted granted Critical
Publication of FR3108360B1 publication Critical patent/FR3108360B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
    • F16F15/322—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels the rotating body being a shaft
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Abstract

L’invention concerne un procédé d’équilibrage d’une pièce tournante (3) de turbomachine pour aéronef, le procédé comprenant les étapes consistant à :a) installer la pièce tournante (3) , qui est équipée d’un cordon d’équilibrage (4) usinable ayant une épaisseur initiale, sur un dispositif d’équilibrage (10) ; l’épaisseur étant mesurée en direction radiale par rapport à un axe (A) de rotation de la pièce tournante (3) ;b) mettre en rotation la pièce tournante (3) suivant ledit axe de rotation (A) ;c) équilibrer la pièce tournante (3) afin de réduire ou supprimer un balourd (33) de la pièce tournante (3), et pendant cette étape c), le procédé comprend une première sous-étape c1) de dépôt d’un matériau d’apport (5) sur au moins une zone (45) du cordon d’équilibrage (4). Figure pour l’abrégé : Figure 3b
FR2002794A 2020-03-23 2020-03-23 Procede et dispositif d’equilibrage d’une piece tournante pour une turbomachine d’aeronef Active FR3108360B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2002794A FR3108360B1 (fr) 2020-03-23 2020-03-23 Procede et dispositif d’equilibrage d’une piece tournante pour une turbomachine d’aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2002794 2020-03-23
FR2002794A FR3108360B1 (fr) 2020-03-23 2020-03-23 Procede et dispositif d’equilibrage d’une piece tournante pour une turbomachine d’aeronef

Publications (2)

Publication Number Publication Date
FR3108360A1 FR3108360A1 (fr) 2021-09-24
FR3108360B1 true FR3108360B1 (fr) 2023-04-14

Family

ID=70295542

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2002794A Active FR3108360B1 (fr) 2020-03-23 2020-03-23 Procede et dispositif d’equilibrage d’une piece tournante pour une turbomachine d’aeronef

Country Status (1)

Country Link
FR (1) FR3108360B1 (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6354780B1 (en) * 2000-09-15 2002-03-12 General Electric Company Eccentric balanced blisk
DE102004037608A1 (de) * 2004-08-03 2006-03-16 Rolls-Royce Deutschland Ltd & Co Kg Unwuchtkompensation von rotierenden Bauteilen
DE102008034342A1 (de) * 2008-07-23 2010-01-28 Continental Mechanical Components Germany Gmbh Verfahren zum Betriebswuchten eines Abgasturboladers mit aktiver magnetischer Lagerung
GB201210870D0 (en) * 2012-06-20 2012-08-01 Rolls Royce Plc Rotor balancing method
EP3192966B1 (fr) * 2016-01-14 2021-05-19 MTU Aero Engines AG Rotor pour une turbomachine axiale avec une bride d'équilibrage orientée axialement et compresseur

Also Published As

Publication number Publication date
FR3108360A1 (fr) 2021-09-24

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