Majority of helicopters have single main lifting rotor, and tail rotor which compensates main rotor torque and is used for directional control; design features of tail rotor; summarized classification of various vibration problems pointing out types of divergent vibrations, resonances and instabilities; types of instability and resonance which may occur; means used to predict and avoid such vibrations include various calculations in design stage and special test stands for development work; substantiation tests enable flight tests to be undertaken with tail rotor free from divergent vibrations.


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    Titel :

    Divergent vibration in helicopter tail rotors


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Normand, Y. (Autor:in)

    Kongress:

    SAE Meeting ; 1965 Vibrations



    Erscheinungsdatum :

    1965


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Divergent Vibration in Helicopter Tail Rotors

    Normand, Y. | SAE Technical Papers | 1965


    Active vibration isolation of helicopter rotors

    Smollen, L.E. / Marshall, P. / Gabel, R. | Engineering Index Backfile | 1962


    Flight performance of helicopter tail rotors with extendable chord

    Yang, Kelong / Han, Dong | SAGE Publications | 2022


    Tail Rotors

    Online Contents | 1994


    Tail Rotors

    Online Contents | 1998