A monitoring system for a dual-stage, stroke activated, mixed fluid gas shock strut may comprise a controller (201), and a tangible, non-transitory memory (208) configured to communicate with the controller. The tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the controller, cause the controller to perform various operations. Said operations may include calculating, by the controller, a compression factor, determining, by the controller, a plurality of compression factors for known oil volumes based on at least one of the primary chamber temperature sensor reading and the shock strut stroke sensor reading, and calculating, by the controller, an oil volume in a primary chamber of the shock strut.


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    Titel :

    DUAL-STAGE, STROKE-ACTIVATED, MIXED FLUID GAS SHOCK STRUT SERVICING MONITORING SYSTEM


    Weitere Titelangaben:

    ZWEISTUFIGES, HUBAKTIVIERTES, MISCHFLUID-GASFEDERBEINWARTUNGSÜBERWACHUNGSSYSTEM
    SYSTÈME DE SURVEILLANCE D'ENTRETIEN D'AMORTISSEUR À GAZ-FLUIDE MÉLANGÉ À DEUX ÉTAGES ET ACTIVÉ PAR COURSE


    Beteiligte:
    FAZELI AMIR (Autor:in) / CEPIC ADNAN (Autor:in) / REBER SUSANNE M (Autor:in)

    Erscheinungsdatum :

    2021-01-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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