FIELD: aviation.
SUBSTANCE: invention relates to aircraft, in particular for structures of combined aerostatic aircraft. Combined vehicle contains a balloon with rigid frame, ballonets and carrier gas, suspension system, cargo-carrying platform with cab controls, motors, electrical and instrumentation. Balloon is composed of two shells of a cylindrical transverse hinge and rotatable and fixed in form of a wing or airfoil as Λ-shaped figures with opened fairing. Suspension system includes rigid and flexible elements and is adapted to transform and fixation. Engines fitted with possibility of changing direction of thrust vector by an angle of between 0° 360° in a vertical plane and fixation. Basing device in a stable position can be carried out on a solid surface of the earth with a bias on water surface, on vertical, rigid construction with a deviation from vertical.
EFFECT: enabling fixation of device is on various surfaces.
4 cl, 8 dwg
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