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Master thesis and internship[BR]- Master's thesis : Vibration under rotor-stator contact - Modelling and experiments correlation[BR]- Integration Internship

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Jamotton, Gilles ULiège
Promoteur(s) : Ponthot, Jean-Philippe ULiège
Date de soutenance : 27-jui-2022/28-jui-2022 • URL permanente : http://hdl.handle.net/2268.2/14361
Détails
Titre : Master thesis and internship[BR]- Master's thesis : Vibration under rotor-stator contact - Modelling and experiments correlation[BR]- Integration Internship
Titre traduit : [fr] Vibration sous contact rotor-stator - Modélisation et corrélation d'essais
Auteur : Jamotton, Gilles ULiège
Date de soutenance  : 27-jui-2022/28-jui-2022
Promoteur(s) : Ponthot, Jean-Philippe ULiège
Membre(s) du jury : Papeleux, Luc ULiège
Charles, Xavier 
Langue : Anglais
Nombre de pages : 95
Mots-clés : [en] Contact
[en] Rotor-Stator
[en] Vibration
[en] Metafor
Discipline(s) : Ingénierie, informatique & technologie > Ingénierie aérospatiale
Institution(s) : Université de Liège, Liège, Belgique
Diplôme : Master en ingénieur civil en aérospatiale, à finalité spécialisée en "aerospace engineering"
Faculté : Mémoires de la Faculté des Sciences appliquées

Résumé

[fr] In 2010, Safran developed a French turbofan called Silvercrest which would power super mid-size to large cabin business jets. During the engine tests, some unexpected vibrations occurred on the booster spool in 2014. These vibrations appeared only for some particular tests and their occurrences were not regular. As the source of this problem was unknown, several hypothesis were explored. The most probable cause was identified to be a contact instability due to the friction between the sealing element of the rotor and the abradable material of the stator. In 2015, partial tests on the booster spool were done to confirm the vibration root cause.
In order to better understand this phenomenon, a numerical model was created in 2017 with the software Metafor to represent this instability induced by contact. Although, the vibrations could be observed in the numerical simulations, they couldn't be compared to experiments because no partial tests on booster spool were available at that time and because the contact conditions on engine tests are difficult to measure.
The goal of this master thesis is to correlate the numerical results with the data from the recent experiments to determine if Metafor can reproduce the same phenomenon. To this aim, the experiments made by Safran Aero Booster are analysed and responses are observed every time a contact interaction appear between rotor and stator. Then, simulations are done with the Metafor model to represent the same phenomenon. The sensitivity of the numerical parameters identifies a strong influence of the damping ratio of the structure and the tangential force due to contact. Finally, these simulations are compared to the experiments and the influence of the rotation speed is highlighted. This work is carried out in collaboration with Safran Aero Booster and the University of Liège that previously developed the numerical model aiming to represent the phenomenon.


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Auteur

  • Jamotton, Gilles ULiège Université de Liège > Master ingé. civ. aérospat., à fin.

Promoteur(s)

Membre(s) du jury

  • Papeleux, Luc ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > LTAS-Mécanique numérique non linéaire
    ORBi Voir ses publications sur ORBi
  • Charles, Xavier Safran group
  • Nombre total de vues 37
  • Nombre total de téléchargements 1










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