IP Library Granted Patent US 8,360,483
Granted Patent B2
US 8,360,483 · App. 12/516,453 · Granted Jan 29, 2013

Door lock for doors of aircraft, especially of helicopters

Inventors: Klaus Koppel (Asbach-Baumenheim, DE); Alexander Rowbut (Aix-en Provence, FR)
Assignee: Eurocopter Deutschland GmbH
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Quick Facts
Patent No.
US 8,360,483
App. No.
12/516,453
Granted
Jan 29, 2013
Kind
B2
Abstract

The invention relates to a door lock comprising a door catch system for double door-type helicopter doors that can, when being closed, additionally be displaced perpendicularly to the plane of the door opening into the closed position (flush fitting). Said door lock comprises a catch element ( 30 ) associated with the latch element ( 31 ) and actively linked therewith, said catch element maintaining the door ‘caught’ directly in front of its locked position when the door is manually closed until the door is translated to its final closed position via the latch element ( 31 ).

Claims (29)

1. Door lock for doors of helicopters, the door lock comprising:

a locking hook attachable to a door structure, the locking hook having a first elongated side surface extending a first length along the locking hook in a lengthwise direction along a first plane;

a catch attachable to a fuselage structure, the catch having a bolt, the bolt having a longitudinal axis located substantially at a right angle to the first plane, the locking hook, by way of a manually activated linkage, being releasably connectable to the bolt to be movable between a blocking position when connected to the bolt and a release position when unconnected to the bolt;

a spring-loaded catch hook connected by a bearing bolt to the locking hook, the catch hook being engageable with the bolt, the catch hook having a second elongated side surface extending a second length along the catch hook in the lengthwise direction along a second plane, the second length being different from the first length;

the locking hook and the catch hook being supported by the bearing bolt equiaxially on a carrier plate, the locking hook and the catch hook each having a hook-shaped opening, the bearing bolt of the catch and locking hooks having a second longitudinal axis; and

a spring-loaded pivoting wedge having a wedge surface and a catch step; and

the spring-loaded pivoting wedge being pivotally supported on the carrier plate by a second bearing bolt having a third longitudinal axis, with the third longitudinal axis of the second bearing bolt being located substantially perpendicular to the second longitudinal axis of the bearing bolt of the catch and locking hooks.

2. Door lock according to claim 1 , wherein the pivoting wedge projects through an opening in the carrier plate into a pivoting region of the locking hook and the catch hook.

3. Door lock according to claim 1 , wherein the wedge surface and the catch step of the pivoting wedge are located on its action surface that faces the end regions of the catch and locking hooks, and wherein the pivoting wedge, on which the torsion spring acts in the counterclockwise direction with respect to the second bearing bolt when the catch step is connected to an extension of the catch hook, blocks the latter in its position in which contact with the stop pin has been made.

4. Door lock according to claim 1 , wherein the free end of the carrier plate facing the catch has a slotted opening, whose rear edge is used as the end stop for the door.

5. Door lock according to claim 1 , wherein the pivoting wedge is supported on a bend of the carrier plate that is used as a flange.

6. Door lock according to claim 5 , wherein the wedge surface and the catch step of the pivoting wedge are located on its action surface that faces the end regions of the catch and locking hooks, and wherein the pivoting wedge, on which the torsion spring acts in the counterclockwise direction with respect to the second bearing bolt when the catch step is connected to an extension of the catch hook, blocks the latter in its position in which contact with the stop pin has been made.

7. Door lock according to claim 2 , wherein the wedge surface and the catch step of the pivoting wedge are located on its action surface that faces the end regions of the catch and locking hooks, and wherein the pivoting wedge, on which the torsion spring acts in the counterclockwise direction with respect to the second bearing bolt when the catch step is connected to an extension of the catch hook, blocks the latter in its position in which contact with the stop pin has been made.

8. Door lock according to claim 2 , wherein the free end of the carrier plate facing the catch has a slotted opening, whose rear edge is used as the end stop for the door.

9. Door lock according to claim 3 , wherein the free end of the carrier plate facing the catch has a slotted opening, whose rear edge is used as the end stop for the door.

10. Door lock according to claim 5 , wherein the free end of the carrier plate facing the catch has a slotted opening, whose rear edge is used as the end stop for the door.

11. Door lock according to claim 6 , wherein the free end of the carrier plate facing the catch has a slotted opening, whose rear edge is used as the end stop for the door.

12. Door lock according to claim 7 , wherein the free end of the carrier plate facing the catch has a slotted opening, whose rear edge is used as the end stop for the door.

13. Door lock for doors of helicopters, the door lock comprising:

a locking hook attachable to a door structure, the locking hook having a first elongated side surface extending a first length along the locking hook in a lengthwise direction along a first plane;

a catch attachable to a fuselage structure, the catch having a bolt, the bolt having a longitudinal axis located substantially at a right angle to the first plane, the locking hook, by way of a manually activated linkage, being releasably connectable to the bolt to be movable between a blocking position when connected to the bolt and a release position when unconnected to the bolt;

a spring-loaded catch hook connected by a bearing bolt to the locking hook, the catch hook being engageable with the bolt, the catch hook having a second elongated side surface extending a second length along the catch hook in the lengthwise direction along a second plane, the second length being different from the first length;

the locking hook and the catch hook being supported by the bearing bolt equiaxially on a carrier plate, the locking hook and the catch hook each having a hook-shaped opening, the bearing bolt of the catch and locking hooks having a second longitudinal axis; and

a spring-loaded pivoting wedge that projects through an opening in the carrier plate into a pivoting region of the locking hook and the catch hook, the spring-loaded pivoting wedge being pivotally supported on the carrier plate by a second bearing bolt having a third longitudinal axis, with the third longitudinal axis of the second bearing bolt being located substantially perpendicular to the second longitudinal axis of the bearing bolt of the catch and locking hooks.

14. Door lock for doors of helicopters, the door lock comprising:

a locking hook attachable to a door structure, the locking hook having a first elongated side surface extending a first length along the locking hook in a lengthwise direction along a first plane;

a catch attachable to a fuselage structure, the catch having a bolt, the bolt having a longitudinal axis located substantially at a right angle to the first side of the locking hook, the locking hook, by way of a manually activated linkage, being releasably connectable to the bolt to be movable between a blocking position when connected to the bolt and a release position when unconnected to the bolt;

a spring-loaded catch hook connected by a bearing bolt to the locking hook, the catch hook being engageable with the bolt, the catch hook having a second elongated side surface extending a second length along the catch hook in the lengthwise direction along a second plane, the second length being different from the first length, the locking hook and the catch hook being supported by the bearing bolt equiaxially on a carrier plate, the locking hook and the catch hook each having a hook-shaped opening, the bearing bolt of the catch and locking hooks having a second longitudinal axis; and

a spring-loaded pivoting wedge that has a wedge surface and a catch step, the spring-loaded pivoting wedge being pivotally supported on the carrier plate by a second bearing bolt having a third longitudinal axis, with the third longitudinal axis of the second bearing bolt being located substantially perpendicular to the second longitudinal axis of the bearing bolt of the catch and locking hooks, wherein the wedge surface and the catch step of the pivoting wedge are located on its action surface that faces the end regions of the catch and locking hooks, and wherein the pivoting wedge, on which the torsion spring acts in the counterclockwise direction with respect to its bearing bolt when the catch step is connected to an extension of the catch hook, blocks the latter in its position in which contact with the stop pin has been made.

Assignments (2)
CHANGE OF NAME Recorded May 2, 2014
From: EUROCOPTER DEUTSCHLAND GMBH
To: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
Reel/Frame 032813/0051 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 6, 2009
From: KOPPEL, KLAUS; ROWBUT, ALEXANDER
To: EUROCOPTER DEUTSCHLAND GMBH
Reel/Frame 023063/0394 →
Priority Claims (1)
DE 10 2006 056 442 · Nov 28, 2006 · national
Continuity (1)
Related Publication 20100064740A1 · Mar 18, 2010