Load e.g. landing gear, hooking case for aircraft, has lock displaced linearly under action of control unit between active position in which lock is placed in contact with hook and inactive position in which lock is remote from hook

摘要

The case has a support hook (4) pivoted around a rotation axis (7) between load hooking and releasing positions. A linear displacement locking mechanism (5) locks the hook in the hooking position. A control unit (6) includes a rotating shaft (35) for controlling the locking mechanism. The mechanism has a sliding lock (17) displaced linearly under the action of the control unit between an active position in which the lock is placed in contact with the hook and an inactive position in which the lock is remote from the hook by releasing the hook.