FIELD: aircraft engineering.
SUBSTANCE: invention relates to VTOL aircraft. Hybrid aircraft includes a storage battery, a control system with a target homing module, body made according to normal "aircraft" aerodynamic configuration, but without tail unit, with straight rectangular wing of flat-convex profile with tips on edges. On the front frontal edge of the wing on support bearings there is a rotary shaft with rigidly fixed on it two electric motors with one or two screws of invariable pitch and with opposite direction of rotation. Rotation of motors through angle of 90 degrees is carried out by a rotary shaft. Suspension devices for bomb weapons are installed on lower flat surface of the hull and straight rectangular wing. On top in the central part of the housing there is an electromagnetic latch for connecting a disposable ring, to which a group of rubber balls inflated with a gas lighter than air is tied for ascent to a given height in a balloon way.
EFFECT: creation of unmanned aerial vehicle of hybrid type, combining properties of balloon, quadcopter, convertiplane, aircraft.
6 cl, 3 dwg
Authors
Dates
2024-03-11—Published
2023-03-28—Filed