Novel aerial survey unmanned aerial vehicle with tilting rotors

The novel aerial survey unmanned aerial vehicle comprises a fuselage body, a rotor shaft is arranged on the fuselage body, a tiltable rotor is arranged on the rotor shaft, a propeller is arranged on the rotor, the propeller is a propeller with five blades, the cutting angle of each blade is 45 degrees, and the cutting angle of each blade is 45 degrees. A torsion shaft used for torsion is arranged at the one-third position of the front end of each paddle, a turboshaft engine is arranged on each rotor wing and adopts a fly-by-wire control mode, a rotor wing arm is arranged in the middle of the fuselage body, a front triangular undercarriage is arranged on the fuselage body, and a rear triangular undercarriage is arranged on the fuselage body. Trapezoidal hanging frames are arranged on the left side and the right side of the bottom of the fuselage body, and hanging points for hanging observation equipment are arranged on the trapezoidal hanging frames, the voyage, the endurance and the load of the unmanned aeria