公开(公告)号：WO2021176271A1

公开(公告)日：2021-09-10

申请号：PCT/IB2020/062583

申请日：2020-12-31

Applicant: LEONARDO S.P.A.

Inventor： PICCOLO, Antonio ,  MASTROIANNI, Gaetana ,  PAPA, Umberto ,  BOTTONE, Emanuele

IPC: B64C5/06 ,  B64C11/00 ,  B64C15/14

Abstract: A fixed-wing aircraft (1) provided with a fuselage (3) which extends along a longitudinal axis (L), a pair of wings, a propulsion system and a vertical stabilizer (5) provided with a vertical drift (6) fixed with respect to the fuselage (3), The drift (6) has a through seat (8) which houses at least one thrust generator (12) adapted to produce in a controllable manner an air flow (F) along a transverse axis (T) from a first side of the drift (6) or from a second side of the drift opposite the first one, producing aerodynamic forces which act on the opposite faces (6a, 6b) of the drift (6) and are used for the directional control of the aircraft (1).