Reduced door opening force and enhanced security flight deck door mechanism
OwnerJames Kunda, Shannon Kupfer +1inventors
InventorsJames Kunda, Shannon Kupfer, Michael Renzelmann
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OwnerJames Kunda, Shannon Kupfer +1inventors
InventorsJames Kunda, Shannon Kupfer, Michael Renzelmann
Estimating the term…
An aircraft door mechanism includes a solenoid connected to a support assembly. The solenoid displaces the latch pin between a solenoid energized and a solenoid de-energized position. A catch assembly rotatably connected to the support assembly is positioned to engage a 3-½ degree or less taper portion of the latch pin in the solenoid energized position. When the latch pin moves to the solenoid de-energized position, a latch bolt supported by the door rotates the catch assembly. The latch bolt includes a distal bulbous end which multiplies the force applied to the door to rotate the catch assembly. If the latch pin is extended, a substantially greater force is required to force the latch pin to the solenoid de-energized position owing to the reduced taper of the latch pin. Authorized door entry is therefore easier and unauthorized door entry is made more difficult.
An aircraft door latch mechanism, comprising:
An aircraft cockpit door mechanism, comprising:
A method for controlling a position of an aircraft cockpit door using a door latch assembly having a rotatable catch and a latch pin connectable to a solenoid, the latch pin including a tapered end;
Dependencies are inferred from the claim text.