The landing gear system disclosed herein may comprise a shrink pump (41) and a shrink valve (44) that are capable of shrinking a landing gear (20) by up to 40% of its available stroke, or more depending on the air spring configuration. The shrink pump (41) may be configured to pump fluid (e.g., a hydraulic fluid) between an oil chamber (38, 39), where hydraulic fluid is likely present and a shrink chamber (36) to shrink the landing gear (20). Moreover, the shrink pump (41) and shrink valve (44) may be part of a strut shrink system (40).


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    Titel :

    Shrink strut landing gear system


    Weitere Titelangaben:

    Schrumpfstreben-Fahrwerksystem
    Système de train d'atterrissage d'entretoise rétractable


    Beteiligte:
    LUCE WILLIAM E (Autor:in)

    Erscheinungsdatum :

    25.05.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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