Force sensor rod

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United States of America Patent

PATENT NO 6830223
SERIAL NO

09716767

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A force sensor rod for an aircraft actuator system. The force sensor rod is constructed from a tube and a force sensing transducer. The force sensing transducer has a body containing a force responsive primary element and electronic circuitry. The force sensing transducer is provided with a protruding end composed of a material relatively harder than the tube material. The threads on the protruding end terminate in a plurality of axially spaced grooves adjacent to the force sensing transducer body and normal to the axis of the force sensing transducer. The tube is threaded onto the protruding end of the force sensing transducer and swaged onto the protruding end by causing the tube material to flow into the grooves.

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Patent Owner(s)

Patent OwnerAddress
TYEE AIRCRAFT3008 100TH STREET SOUTHWEST EVERETT WA 98204

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Moore, Daniel Lee Edmonds, WA 2 24

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