Lock defeating system for an aircraft door
A system and method for defeating a door lock. More specifically, a door having an outside door handle with a key-lock, and having an interior door handle of the type that includes both a paddle along with the handle runs the risk of being left in locked mode in the event of a mechanical malfunction. This problem has been overcome by mechanically linking the paddle on the interior handle to unlatch the key-lock.
1. An aircraft door comprising:
an exterior door handle assembly including a key-operated lock, the key-operated lock being operable to a locked position where an outstanding tab on the key-operated lock is rotated between a first locked position and a second unlocked position;
an interior door handle assembly including a paddle portion and a handle portion, wherein the paddle portion and the handle portion are configured in such a way that the action of operating the handle portion causes the actuation of the paddle portion, the paddle portion being operably linked via a mechanical system to an opposing outwardly extending blocking member;
the blocking member, when the paddle portion is not being actuated by a user, and when the key-operated lock is in the locked position, existing in blocking mode where the outstanding tab overlaps and engages with the blocking member and prevents an opening of the door; and
the blocking member, when the paddle portion is actuated by a user, existing in an unblocked mode where the outstanding tab of the key-operated lock overlaps and engages with the blocking member and does not block opening of the door on an actuation of the handle on the exterior door assembly.
2. The aircraft door of claim 1 wherein the blocking member is a cam on an axis of rotation internal to the door.
3. The aircraft door of claim 1 wherein the mechanical system includes a rod configured to rotate about the longitudinal axis upon activation of the paddle, the rod imparting rotation used in operating the blocking member.
4. The aircraft door of claim 1 wherein the mechanical system includes a shaft with two ends and a centerpoint on each end, configured to rotate on an axis defined by the centerpoints of the ends of the shaft upon activation of the paddle, the shaft imparting rotation used in operating the blocking member.
5. The aircraft door of claim 4 wherein the mechanical system includes an arm that imparts tension into a cable, the cable contributing in imparting rotation of the blocking member.
6. The aircraft door of claim 5 wherein the mechanical system includes a fairlead that the cable slides around to reach a bellcrank which is included in the imparting of rotation to the blocking member.
7. The aircraft door of claim 6 wherein the mechanical system includes a rod which is driven by the bellcrank to contribute to the rotation of the blocking member.
8. The aircraft door of claim 7 wherein the mechanical system includes a seesaw rotating on an axle at a first end, the seesaw being configured to receive pressure from the rod at an intermediate location and cause the axle to operate the blocking member into an unlocked position.
9. The aircraft door of claim 8 wherein the mechanical system includes a tension spring attached to a second end of the seesaw, the tension spring having a tension level, the tension spring biasing the blocking member towards blocked mode when the paddle is not being depressed by a user to overcome the tension level provided by the tension spring.
10. An aircraft door comprising:
an exterior handle system having a lock tab which rotates to catch on an axially mounted blocking member when in locked mode and is rotatable to an unlocked mode where the tab does not catch on the blocking member;
an interior handle system including a paddle which is operated by a user to gain the ability to operate a handle in the interior handle system, wherein the paddle and the handle are configured in such a way that the action of operating the handle portion causes the actuation of the paddle portion; and
the paddle rotating on a shaft, the shaft configured to impart mechanical rotation to the blocking member via a mechanical system.
11. The aircraft door of claim 10 wherein the blocking member is a cam on an axis of rotation internal to the door.
12. The aircraft door of claim 10 wherein the mechanical system includes an arm on the shaft imparts tension into a cable, the cable contributing to impart rotation of the blocking member.
13. The aircraft door of claim 12 wherein the cable slides around a fairlead in imparting rotation to the blocking member.
14. The aircraft door of claim 13 wherein the cable, after sliding around the fairlead, rocks a bellcrank to impart rotation to the blocking member.
15. The aircraft door of claim 14 wherein the mechanical system includes a rod which is driven by the bellcrank to contribute to the rotation of the blocking member.
16. The aircraft door of claim 15 wherein the mechanical system includes a seesaw which operates on an axle, the seesaw being rocked at a first end by the rod resulting in a rotation of the axle on which the blocking member is rotatable into an unlocked position.
17. The aircraft door of claim 16 wherein a tension spring is attached to a second end of the seesaw, the tension spring having a tension level, the tension spring biasing the blocking member towards blocked mode when the paddle is not being depressed by a user.
18. A lock-defeat process for use with a door having a first handle having a key-lock arrangement on a first side of the door and a paddle associated with a second handle existing on a second side of the door, the process comprising:
mechanically linking the paddle associated with the second handle to the key-lock associated with the first handle such that the operation of the paddle maintains an unlatching of the key-lock, and
configuring the paddle and the second handle in such a way that the action of operating the second handle causes the actuation of the paddle.
19. The lock-defeat process of claim 18 comprising:
accepting rotation from the paddle to rotate a cam away from a blocked position to defeat the key-lock.
20. The process of claim 19 comprising:
accomplishing the accepting step by receiving drive from the paddle into an intermediate portion of a seesaw rotating on an axle, and
biasing an opposite end of the seesaw using a tension spring to return the cam to a blocking position upon a release of the paddle.