An aircraft comprising a mechanical connection device including a body that extends along a longitudinal axis. The body comprises two opposite end portions disposed along the longitudinal axis and adapted to receive external axial loads in compression and in tension, a spring member that is adapted to be compressed axially, and a mechanism which, in the event of external axial loads in compression or in tension on the end portions, is able to transmit to the spring member compression forces oriented in opposite directions according to whether the external axial loads are in compression or in tension. This device forms a flexible connection that accommodates equally well external loads in compression and in tension.


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    Title :

    DISPOSITIF DE LIAISON MECANIQUE


    Contributors:

    Publication date :

    2016-08-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge





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