The invention provides a short-distance
takeoff ideal scheme of a running take-off
airplane. The core technology is that a
runway is divided into a fixed part and a dynamic part, and the fixed part is closely connected with the dynamic part, so that the
airplane is static relative to the fixed
runway when running on the dynamic
runway and enters into the fixed runway till being accelerated at a preset speed on the dynamic runway, therefore, the
airplane can realize the short-distance
takeoff under the status of high initial speed and large
kinetic energy. The airplane not only meets the best requirements of the aircraft carrier airplane such as short-distance
takeoff, full-load takeoff and full-oil takeoff, but also has the capability of short-distance landing. A crawler type integrated dynamic runway has the functions of short
takeoff and landing, can be used for preventing the airplane from rushing out of the runway in a land
aerodrome, can be used for building a military field
aerodrome, can be used for building a temporary
takeoff and landing point for the vehicle-mounted (carrier-based) military aircraft, possibly brings the development direction of the
miniaturization and the
submarine trend of the aircraft carrier, and possibly brings the great change of an air
operation mode. The airplane jointly uses three schemes such as a crawler type integrated dynamic runway, a three-point type synchronous running wheel short-distance take-off airplane, a straight line type synchronous column wheel short-distance take-off airplane, and the like.