An active control undercarriage for the alleviation of aircraft landing gear and structural loads during operation on rough runway surfaces is described. For quantitative determination of the improvements obtained with an active control undercarriage compared with conventional landing gear systems, aircraft taxiing is realistically simulated by means of a laboratory test set-up especially designed for this kind of testing.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Actively Damped Landing Gear System


    Beteiligte:
    R. Freymann (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Actively Damped Landing Gear System

    Freymann, R. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research and Development; Structures and Materials Panel | British Library Conference Proceedings | 1991


    Actively Controlled Landing Gear for Aircraft Vibration Reduction

    Horta, Lucas G. / Daugherty, Robert H. / Martinson, Veloria J. | NTRS | 1999


    Modeling and Validation of a Navy A6-Intruder Actively Controlled Landing Gear System

    Horta, Lucas G. / Daugherty, Robert H. / Martinson, Veloria J. | NTRS | 1999


    Modeling and Validation of a Navy A6-Intruder Actively Controlled Landing Gear System

    L. G. Horta / R. H. Daugherty / V. J. Martinson | NTIS | 1999


    LANDING GEAR DOOR SYSTEM FOR LANDING GEAR COMPARTMENT

    SEAN C WEBB | Europäisches Patentamt | 2022

    Freier Zugriff