| 摘要 |
An aeronautical body is enabled for carrying personnel, and mounted in laterally extending positions from the side surfaces of the body are a pair of medially placed main wings and a pair of proximally placed canard wing tips. In spaced apart proximity to the side and top surfaces of the body, and mounted therefrom, a pair of horizontal stabilizer wings and a propulsion device are placed. A pair of helicopter rotor assemblies are mounted at mutually divergent angles such that a pair of rotor blades are enabled for rotation without mutual interference. The body is mounted on wheels enabled for supporting, propelling and steering the apparatus in movements on a hard surface.
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