FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, particularly to the rotorcrafts designs. Convertiplane comprises fuselage with cockpit of pilots, stabilizer, keel, wings with steering surfaces, made with possibility of maintaining course stability and controllability in aircraft mode and arranged along aircraft layout, a rotor column connected to the fuselage by means of a hinge, which enables to change the angle of rotation of the column in range of 100°+-10° relative to horizon. Wings are installed near fuselage center of gravity on both sides. Rotor column is connected to the fuselage at the center of its gravity with the possibility of being installed in vertical position at takeoff and landing and installation in aircraft mode in horizontal position above fuselage synchronously with wings, with accommodation of rotor with blades in front of fuselage nose. Rotor blades are made with jet engines of their rotation, and conversion is performed by rotor controlled by swash plate and common pitch mechanism.
EFFECT: higher efficiency of convertoplan due to reduced weight of power plant and propulsor.
1 cl, 2 dwg
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Authors
Dates
2019-11-11—Published
2018-11-08—Filed