Measuring and testing – Navigation – Take-off and landing monitors
Patent
1984-02-13
1986-03-04
Chin, Peter
Measuring and testing
Navigation
Take-off and landing monitors
7386204, G01C 2100
Patent
active
045733511
ABSTRACT:
A hub moment sensor is disclosed for an aircraft having a horizontal rotor, a rotor fixed mast for supporting the rotor above the aircraft body, and a support ring formed on the aircraft body for attachment to the rotor fixed mast. The sensor comprises an annular flange formed on the end of the rotor fixed mast remote from the rotor, and coupling means for securing the flange to the support ring, the coupling means including stress measuring means, whereby the moments acting on the aircraft may be sensed.
Chin Peter
Litton Systems Inc.
Ribando Brian L.
LandOfFree
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