A rotorcraft includes a fuselage with at least one rotor assembly coupled thereto. A drivetrain provides rotational energy to the rotor assembly. The drivetrain includes an engine and a gearbox having a gearbox housing. A gearbox cooling fin array including a plurality of cooling fins is bonded to the gearbox housing with a thermal interface material. The gearbox cooling fin array is configured to dissipate heat generated by the gearbox during operation of the rotorcraft.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Bondable Cooling Fin Arrays for Use on Aircraft Gearboxes


    Beteiligte:
    GILLILAND COLTON (Autor:in) / HENRY TYSON T (Autor:in)

    Erscheinungsdatum :

    2020-12-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Bondable fitting

    RICHARD DOBBIN / MICHAEL GORDON | Europäisches Patentamt | 2018

    Freier Zugriff


    Autonomous Emergency Lubrication of Aircraft Gearboxes

    OLSON ERIC STEPHEN / TIPRIGAN EZRA MIKE | Europäisches Patentamt | 2024

    Freier Zugriff


    Manufacturing considerations related to aircraft gearboxes

    McDade, J.N. / Collin, G.B. | Tema Archiv | 1985