Locking mechanism for an aircraft door and method for the locking of an aircraft door

摘要

A locking mechanism for an aircraft door includes a plurality of frame-side fittings and a plurality of door-side fittings. Each frame-side fitting includes a pin with an eccentric rotary cylinder mounted on each pin. Each door-side fitting includes an eccentric rotary latch configured to encompass at least a section of a corresponding rotary cylinder. Also a method of locking a door using the locking mechanism.

主权项

1. A locking mechanism for an aircraft door, the locking mechanism comprising:
a plurality of frame-side fittings, each frame-side fitting including a pin; an eccentric rotary cylinder mounted on each pin the rotary cylinder having an outer periphery; and a plurality of door-side fittings, each door-side fitting including an eccentric rotary latch having an inner periphery, the rotary latch being configured to encompass at least a section of a corresponding rotary cylinder, and being configured to run with its inner periphery onto the outer periphery of the rotary cylinder through a rotary movement and to drive the rotary cylinder to execute a rotation, such that a moment is introduced into the locking mechanism, through which the rotary cylinder is continuously pushed into the locking position.