A pitch stabilizer with box configuration suitable for providing stability to a rotorcraft comprising a vertical mid-plane and a fuselage; the pitch stabilizer comprising one or two pitch stabilizing assemblies, with no more than one pitch stabilizing assembly on each side of the vertical mid-plane, wherein each pitch stabilizing assembly comprises upper pitch stabilizing means, lower pitch stabilizing means and a wing tip element.
ADVANCED PITCH STABILIZER
2015-10-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Pitch stabilizer and rotary-wing aircraft equipped with such stabilizer
European Patent Office | 2015
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