A pitch stabilizer (10) with box configuration suitable for providing stability to a rotorcraft comprising a vertical mid-plane (15) and a fuselage (14); the pitch stabilizer (10) comprising one or two pitch stabilizing assemblies, with no more than one pitch stabilizing assembly on each side of the vertical mid-plane (15), wherein each pitch stabilizing assembly comprises upper pitch stabilizing means (11), lower pitch stabilizing means (12) and a wing tip element (13).
Advanced pitch stabilizer
Erweiterter Steigungsstabilisator
Stabilisateur de pas avancé
2017-05-24
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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