A method of automatically adjusting the lift of a hybrid rotorcraft and an associated hybrid rotorcraft

摘要

The present invention relates to a method for automatically adjusting the lift of a hybrid rotorcraft (1), said hybrid rotorcraft (1) comprising a fuselage (2) and at least two half-wings (11, 11 ') positioned so as to on either side of an anteroposterior median plane of said fuselage (2), said at least two half-wings (11, 11 ') comprising on the one hand at least one left half-wing (11) comprising a left fixed structure (13) secured to said fuselage (2) and at least one left flap (12) movable relative to said left fixed structure (13) and on the other hand at least one right wing half (11 ') comprising a right fixed structure (13 ') secured to said fuselage (2) and at least one right flap (12') movable relative to said straight fixed structure (13 '). Such a method makes it possible to determine at least a first steering angle setpoint δw1 of said at least one left flap (12) relative to said left fixed structure (13) and at least one second steering angle setpoint δw2 of said at least a right flap (12 ') relative to said straight fixed structure (13') ,. Abstract figure: Figure 1