Semi-split type hovercar

The utility model provides a semi-split type hovercar which comprises a hovercar body and a general flying module, the flying module is located above the hovercar body, and the hovercar body and the flying module are connected through two connecting modes at the same time, namely separable rigid mechanical structure connection and flexible mooring rope connection. The flight module comprises a central connecting mechanism and a plurality of rotor wing lifting devices distributed around the connecting mechanism, the rotor wings are distributed in a bilateral symmetry mode, the height differencebetween the upper position and the lower position exists between every two adjacent left-right or front-back rotor wings, and each pair of two rotor wings in bilateral symmetry can be integrally folded to the middle position to form a single coaxial rotor wing. The unmanned aerial vehicle solves the contradiction between the size of the vehicle body and the aerodynamic efficiency, has the capabilities of ground driving, aerial flight and vertical take-off and landing, can take off and land in a narrow space, has higher power load and aerodynamic efficiency, and has higher voyage and flight efficiency.