| 摘要 |
The invention relates to the field of aviation, and specifically to aircraft structures. The present hybrid aircraft comprises an aerostat with a rigid frame, ballonets with helium, a suspension system, and a bearing platform with a cargo/passenger cabin. The cabin includes controls, engines, electrical equipment and measurement devices. The aerostat is composed of two envelopes connected by a cylindrical hinge and provided with affixing elements, controlling the rotation of which allows for changing and securing the aerostat in the form of a wing or in the form of an A-shape with an opened fairing. The suspension system includes rigid and flexible connections and is capable of being transformed and secured. The stationing and securing of the device in a stable position can be carried out on a sloped solid ground surface, on a water surface, or on a vertical structure. |
