A cargo restraint system may comprise a restraint and an actuator shaft configured to rotate the restraint between a raised position and a stowed position. The restraint may include a head configured to rotate about an axis and a plunger configured to translate between an engaged state and a disengaged state. When the plunger is in the engaged state, the head is rotationally coupled to the actuator shaft. When the plunger is in the disengaged state, the head can rotate independently of the actuator shaft.


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    Title :

    CARGO RESTRAINT SYSTEM WITH INDIVIDUALLY RETRACTABLE RESTRAINTS



    Publication date :

    2023-02-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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