FIELD: aviation.
SUBSTANCE: invention relates to aircraft chassis. Aircraft chassis assembly (10) contains main bearing rack (12), strut (18), lock link (26), unlocking drive (32). Lock link (26) can be moved for taking the first locking position in order to prevent the movement of strut (18), when main rack (12) is in a released position, and the second locking position in order to prevent the movement of main rack (12), when it is in a retracted position. Unlocking drive (32) has the first end pivotally connected to first strut element (18a) at the first point of drive rotation, and the second end pivotally connected to lock link (26) at the second point of drive rotation. The drive is made with the possibility of moving the lock link from the first locking position to a passive position by means of extension or retraction, and with the possibility of moving the lock link from the passive position to the second locking position by means of the same extension or retraction.
EFFECT: simplification of the design of the chassis assembly is achieved.
15 cl, 8 dwg
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