The disclosed sensor includes a frame having a base and a plurality of arms integral with the base. The arms are biased to a relaxed position, which may be an extended position. A fuse is fastened between the arms to hold the arms in a non-relaxed position. When incorporated into an aircraft, for example, the disclosed sensor may be connected to a first panel, and a pin connected to a second panel may be positioned between the arms.
Cantilevered differential motion sensor and associated frame
2015-08-11
Patent
Electronic Resource
English
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