This paper presents experimental results on the non-linear vibration response of a rotating assembly comprising a rotor, flexible bearing housing and oil film damper. For the latter, due consideration is given to the effects of oil-supply pressure, film-rupture pressure and end sealing. The results are compared with predictions based on the Harmonic Balance principle described in a complementary paper (1).


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    Titel :

    Experimental Investigation into the Vibration Response of an Aero-Engine Rotor-Damper Assembly


    Beteiligte:
    Levesley, M C (Autor:in) / Holmes, R (Autor:in)


    Erscheinungsdatum :

    01.01.1994


    Format / Umfang :

    15 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch