A health and monitoring system or "HUMS" (20a, 20b) mounted within a hollow structural subassembly (12) of an aircraft landing gear assembly (10), the subassembly having an access port (16) for access to the HUMS without requiring disassembly of the structural subassembly so as to require jacking up the aircraft.


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    Titel :

    AIRCRAFT LANDING GEAR ASSEMBLY INCLUDING A HEALTH AND USAGE MONITORING SYSTEM (HUMS) AND METHOD


    Weitere Titelangaben:

    FLUGZEUGLANDEFAHRWERKANORDNUNG MIT GESUNDHEITS- UND GEBRAUCHSÜBERWACHUNGSSYSTEM (HUMS) UND VERFAHREN
    ENSEMBLE DE TRAIN D'ATTERRISSAGE D'AÉRONEF COMPRENANT UN SYSTÈME ET UN PROCÉDÉ DE SURVEILLANCE DE SANTÉ ET D'UTILISATION (HUMS)


    Beteiligte:

    Erscheinungsdatum :

    26.04.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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