Patent ID: 11926406
Assignee: AIRBUS OPERATIONS LIMITED
Field: Transport (Mechanical engineering)
Classification: CPC B  E  F | IPC B  E

Claim 8:
9. An aircraft hatch, comprising:
a hatch panel with hatch bulkheads and hatch skin elements;
a hatch locking device according to claim 1 which is mounted in the hatch panel;
a hatch frame region with a locking bolt which is driven via a two-way linear actuator and is guided along the bolt receptacle axis in a frame bolt receptacle;
a frame eccentric bush which is connected to a hatch frame bulkhead; and
a frame inner lining which is introduced into the frame eccentric bush and in which an inner conical shell face of a frame conical pressing sleeve is in displaceable engagement with an outer conical shell face of a frame conical clamping sleeve, and in which frame linear actuators which are attached on in each case two opposite sides of the frame conical pressing sleeve are configured to displace the frame conical pressing sleeve along the bolt receptacle axis with respect to the frame conical clamping sleeve to clamp in or release the locking bolt.