FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, particularly, to vertical take-off and landing of an aircraft. Convertible plane contains a fuselage, pair of wings – front and rear, power plants containing engines and propellers, keel, chassis, pylons, made with the possibility of rotation. Two lifting power plants are located on pylons with two degrees of freedom – in the yaw and pitch angles, on the sides of the fuselage with the possibility of fixing the position and cleaning during horizontal flight forward or backward in the fuselage niches. Marching power plant installed on the pylon with one degree of freedom in the pitch angle, with the possibility of fixing the position, or made completely fixed, with the possibility of being placed either in the nose or tail fuselage, as well as on the leading or trailing edges of the keel.
EFFECT: increased reliability, resource, increasing the range of the convertible plane are provided.
1 cl, 4 dwg
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Authors
Dates
2019-03-21—Published
2018-03-05—Filed