A door for an aircraft includes a first panel (58) divisible into at least two first slats (64-70) that are releasable connected to one another, a first tensioning cable (100) attached between the at least two first slats, and a first tensioner (124) connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments.

    La présente invention se rapporte à une porte pour un aéronef, ladite porte comprenant un premier panneau qui peut être divisé en au moins deux premiers ailerons qui sont raccordés de manière amovible les uns aux autres, un premier câble de tension fixé entre les au moins deux premiers ailerons, et un premier tensionneur raccordé au premier câble de tension et qui est utilisé pour appliquer une première tension à ce dernier, ce qui permet au premier câble de tension de supporter ensemble les au moins deux premiers ailerons afin de former le premier panneau et de relâcher la première tension du premier câble de tension lors de l'apparition d'une action de relâchement, ce qui permet de dissocier les uns des autres les au moins deux ailerons comme les premiers fragments de panneau.


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    Title :

    DOOR FOR AN AIRCRAFT


    Additional title:

    PORTE POUR UN AERONEF


    Contributors:

    Publication date :

    2021-07-20


    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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