Invention Grant
- Patent Title: Aircraft door actuator mounting assembly
- Patent Title (中): 飞机门执行器安装组件
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Application No.: US12355347Application Date: 2009-01-16
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Publication No.: US08256311B2Publication Date: 2012-09-04
- Inventor: David A. Payne , Jim Kern , Stephen Birn
- Applicant: David A. Payne , Jim Kern , Stephen Birn
- Applicant Address: US NJ Morristown
- Assignee: Honeywell International Inc.
- Current Assignee: Honeywell International Inc.
- Current Assignee Address: US NJ Morristown
- Agency: Ingrassia Fisher & Lorenz, P.C.
- Main IPC: F16H25/08
- IPC: F16H25/08

Abstract:
An actuator mounting assembly includes a cap, a rod, a spring mechanism, and a switch assembly. The cap is adapted to couple to an actuator. The rod extends through the cap and includes a first end adapted to extend through the actuator and a second end adapted to attach to a fixed location. The spring mechanism is disposed in the cap cavity, is compressible, and has a predetermined preload. The switch assembly is disposed in the cap and adapted to sense relative positioning between the rod and the cap and to provide signals based on the sensed relative positioning. When the rod and the cap are in a first relative position, the switch assembly provides a first signal to the actuator to allow the cap to move axially relative to the rod, but when in a second relative position, the switch assembly discontinues providing the first signal to the actuator.
Public/Granted literature
- US20100180432A1 ACTUATOR MOUNTING ASSEMBLIES, ACTUATOR ASSEMBLIES, AND METHODS OF ADJUSTING AN ACTUATOR Public/Granted day:2010-07-22
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