A self-powered drone flying car for land and air, comprising: a riding cylindrical body having a spherical shape to provide a space for flying, steering, transporting, and controlling; four auxiliary wheels attached to a lower both sides of the riding cylindrical body to vertically stand and move the riding cylindrical body; a shock absorber frame device (140,160,162) attached to each of the auxiliary wheels and upper and lower vertices of the riding cylindrical body to absorb a shock generated during driving; a fan cylinder device (150,161,162) fixed and attached to the shock absorber frame device to generate a wind power; a self-power generator (161,170,200) configured to generate electricity by using a wind power generated from a fan membrane mounted and moved in the fan cylinder and a movement force of a fan membrane moving pole; a rotation load wheel frame device having a shape of surrounding an outer portion of the riding cylindrical body to provide a rotation load to a driving wheel connected thereto; a direction conversion device mounted to each of front, rear, and middle portions of the riding cylindrical body and connected with the rotation load wheel frame device to convert a direction of each of the rotation load wheel frame device and the driving wheel into left and right directions; a driving gear device mounted to each of front, rear, and middle portions of the riding cylindrical body and then connected to a driving chain that is a driving transmission unit formed on an inner frame of the driving wheel; five drone wing devices connected to an upper portion of the riding cylindrical body to perform a vertical take-off and landing and a flight and vertically folded when driving on the ground or not used; a parachute capsule device formed on the upper portion of the riding cylindrical body to unfold a parachute contained therein, thereby performing a soft landing in case of emergency; an intermediate connection attaching and detaching frame device configured to connect and detach the drone wing device and the parachute capsule device formed on the upper portion of the riding cylindrical body therebetween. a riding cylindrical body having a spherical shape to provide a space for flying, steering, transporting, and controlling; four auxiliary wheels attached to a lower both sides of the riding cylindrical body to vertically stand and move the riding cylindrical body; a shock absorber frame device (140,160,162) attached to each of the auxiliary wheels and upper and lower vertices of the riding cylindrical body to absorb a shock generated during driving; a fan cylinder device (150,161,162) fixed and attached to the shock absorber frame device to generate a wind power; a self-power generator (161,170,200) configured to generate electricity by using a wind power generated from a fan membrane mounted and moved in the fan cylinder and a movement force of a fan membrane moving pole; a rotation load wheel frame device having a shape of surrounding an outer portion of the riding cylindrical body to provide a rotation load to a driving wheel connected thereto; a direction conversion device mounted to each of front, rear, and middle portions of the riding cylindrical body and connected with the rotation load wheel frame device to convert a direction of each of the rotation load wheel frame device and the driving wheel into left and right directions; a driving gear device mounted to each of front, rear, and middle portions of the riding cylindrical body and then connected to a driving chain that is a driving transmission unit formed on an inner frame of the driving wheel; five drone wing devices connected to an upper portion of the riding cylindrical body to perform a vertical take-off and landing and a flight and vertically folded when driving on the ground or not used; a parachute capsule device formed on the upper portion of the riding cylindrical body to unfold a parachute contained therein, thereby performing a soft landing in case of emergency; an intermediate connection attaching and detaching frame device configured to connect and detach the drone wing device and the parachute capsule device formed on the upper portion of the riding cylindrical body therebetween.