NASA NTRS · 19810010561
Compensating linkage for main rotor control
Abstract
A compensating linkage for the rotor control system on rotary wing aircraft is described. The main rotor and transmission are isolated from the airframe structure by clastic suspension. The compensating linkage prevents unwanted signal inputs to the rotor control system caused by relative motion of the airframe structure and the main rotor and transmission.
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Jeffery, P. A. E., Huber, R. F.. 1981-01-20. Compensating linkage for main rotor control. https://ntrs.nasa.gov/citations/19810010561
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