A monitoring system for a dual-stage, separated gas/fluid shock strut (100) 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 determining, by the controller, a shock strut stroke at which a secondary chamber of the shock strut is activated, calculating, by the controller, a volume of oil in an oil chamber (150) of the shock strut, calculating, by the controller, a volume of gas in a primary chamber (130) of the shock strut, and calculating, by the controller, a volume of oil leaked into the primary chamber of the shock strut.


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    Titel :

    DUAL-STAGE, SEPARATED GAS/FLUID SHOCK STRUT SERVICING MONITORING SYSTEM USING TWO PRESSURE/TEMPERATURE SENSORS


    Weitere Titelangaben:

    ZWEISTUFIGES GETRENNTES GAS-/FLUID-FEDERBEIN-WARTUNGSÜBERWACHUNGSSYSTEM MIT ZWEI DRUCK-/TEMPERATURSENSOREN
    SYSTÈME DE SURVEILLANCE D'ENTRETIEN À JAMBE D'AMORTISSEUR À GAZ/FLUIDE SÉPARÉE À DEUX ÉTAGES UTILISANT DEUX CAPTEURS DE PRESSION/TEMPÉRATURE


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

    Erscheinungsdatum :

    2020-04-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    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 / F16F SPRINGS , Federn / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



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