A rotary wing aircraft (100) extending along an associated roll axis (R) between a nose region (101) and an aft region (102) and that comprises a fuselage (110) with a front section (112) and a rear section (114), the rotary wing aircraft (100) comprising: a main rotor (120) that is rotatably mounted at the front section (112), and a stabilizer arrangement (130) that is arranged at the rear section (114) in the aft region (102), wherein the rear section (114) extends between the front section (112) and the stabilizer arrangement (130) and comprises an asymmetrical cross-sectional profile (190) in direction of the associated roll axis (R).
A ROTARY WING AIRCRAFT WITH A STABILIZER ARRANGEMENT
DREHFLÜGELFLUGZEUG MIT EINER STABILISATORANORDNUNG
AÉRONEF À VOILURE TOURNANTE COMPORTANT UN AGENCEMENT DE STABILISATEUR
2023-11-08
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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