A hard-landing detection system includes a wheel assembly (106), a shock strut (104) mechanically coupled to the wheel assembly and to landing gear structure of the landing gear assembly, a controller (230) having a processor, and a tangible, non-transitory memory configured to communicate with the processor. The tangible, non-transitory memory has instructions stored thereon that, in response to execution by the processor, cause the hard-landing detection system to perform operations that include detecting, by the processor, a landing event and determining, by the processor, whether the landing event is hard. The hard-landing system may further include a stroke position sensor (116) and detecting the landing event may include using the stroke position sensor to measure a stroke profile of the shock strut. Further, determining whether the landing event is hard may include comparing, by the processor, the stroke profile of the shock strut to a predetermined maximum shock strut stroke.


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    Title :

    HARD-LANDING DETECTION SYSTEM


    Additional title:

    HARTLANDUNGSERKENNUNGSYSTEM
    SYSTEME DE DETERMINATION D'ATTERRISSAGE DUR


    Contributors:
    CEPIC ADNAN (author) / FAZELI AMIR M (author) / REBER SUSANNE (author)

    Publication date :

    2020-11-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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