Invention Grant
- Patent Title: Reduced door opening force and enhanced security flight deck door mechanism
- Patent Title (中): 减少门开启力和增强安全驾驶舱门机构
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Application No.: US11923238Application Date: 2007-10-24
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Publication No.: US07770949B2Publication Date: 2010-08-10
- Inventor: James J. Kunda , Shannon J. Kupfer , Michael E. Renzelmann
- Applicant: James J. Kunda , Shannon J. Kupfer , Michael E. Renzelmann
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: Harness, Dickey & Pierce, P.L.C.
- Main IPC: E05B15/02
- IPC: E05B15/02 ; E05C1/06

Abstract:
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 3½ 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.
Public/Granted literature
- US20080135684A1 Reduced Door Opening Force and Enhanced Security Flight Deck Door Mechanism Public/Granted day:2008-06-12
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