The effort during Phase I of the contract included detailed design of a composite wheel assembly to function structurally and mechanically in a manner identical to the existing metal braked main landing gear wheel for the T-39 aircraft. The design and analysis of the graphite composite landing gear wheel was based on demonstrated material properties. A thermal analysis of the composite structure showed the maximum wheel temperature to be 406 F adjacent to the steel brake keys (inner wheel half) and 223 F on the outer wheel half. Hercules 4397/AS resin system was selected for the inner wheel half and 3501/AS for the outer half. During Phase II, one inner and two outer wheel halves were fabricated. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Graphite Composite Aircraft Landing Gear Wheel


    Erscheinungsdatum :

    1976


    Format / Umfang :

    94 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aircraft landing gear aircraft wheel synchronizer

    YANG AO | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft landing gear wheel-drive system

    LO CHARLES / STEVES ALLAN | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT LANDING GEAR WHEEL WITH INTEGRAL GEAR DRIVE

    CHRISTENSEN DONALD JEFFREY / MITCHELL ROBERT | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft landing gear wheel with integral gear drive

    CHRISTENSEN DONALD JEFFREY / MITCHELL ROBERT | Europäisches Patentamt | 2016

    Freier Zugriff

    AIRCRAFT LANDING GEAR WHEEL WITH INTEGRAL GEAR DRIVE

    CHRISTENSEN DONALD JEFFREY / MITCHELL ROBERT | Europäisches Patentamt | 2016

    Freier Zugriff