The cable flight control systems are commonly used for the control of small airplanes. In these systems, the cables are the only elements transmitting loads from the pilot to the control surfaces. During a flight the cables are moving through pulleys and are subjected to variable loads. A simple analysis of stress in the cable shows that the stress generated by the cyclical bending on the pulleys causes the fatigue of the wires.


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    Titel :

    The Fatigue Life of Cables in Aircraft Flight Control Systems


    Beteiligte:
    Kubryn Mariusz (Autor:in) / Gruszecki Henryk (Autor:in) / Pieróg Leszek (Autor:in) / Chodur Jerzy (Autor:in) / Pietruszka Janusz (Autor:in) / Brzęczek Józef (Autor:in)


    Erscheinungsdatum :

    2018




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    Developments in aircraft control cables

    Beed, C.F. | Engineering Index Backfile | 1941





    Aircraft Flight Control

    KNEUPER JEREMY JOSEPH / LANIER JOHN ROBERT / DECKER JASON MICHAEL | Europäisches Patentamt | 2016

    Freier Zugriff