The invention relates to a vibration absorbing structure, an inertia measurement structure with the vibration absorbing function and an aircraft. The vibration absorbing structure is used for absorbing vibration of an inertia measurement unit in the aircraft and comprises a spring stabilizing assembly and a damping body, wherein the spring stabilizing assembly is arranged between the inertia measurement unit and a frame structure of the aircraft so as to make the inertia measurement unit keep tending to be stable in a preset state, and the damping body is arranged between the inertia measurement unit and the frame structure of the aircraft so as to absorb vibration energy output by the aircraft to the inertia measurement unit. By means of the technical scheme, influences of vibration on the inertia measurement unit can be stopped stably for a long time.


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    Titel :

    Vibration absorbing structure, inertia measurement structure with vibration absorbing function and aircraft


    Beteiligte:
    CHEN ZHIMING (Autor:in) / CAI WEI (Autor:in) / CHE JIANMING (Autor:in)

    Erscheinungsdatum :

    14.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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