High-energy rotor blasting risk evaluation method based on digital model

The invention discloses a high-energy rotor blasting risk evaluation method based on a digital model. Comprising the following steps: step 1, in a scheme design stage, carrying out risk pre-evaluation by utilizing a digital prototype model in the scheme design stage; step 2, in a preliminary design stage, carrying out risk evaluation by utilizing the digital prototype model in the preliminary design stage; and 3, in a detailed design stage, carrying out final risk evaluation by utilizing the digital prototype model in the detailed design stage. The method closely fits the detail degree of digital prototype data in each stage of airplane development, non-inclusive high-energy rotor blasting risk analysis is carried out in stages, the characteristic that traditional non-inclusive high-energy rotor blasting risk analysis is not high in operability is avoided, the arrangement risk of an airplane can be researched and judged in advance, and the reliability of the airplane is improved. And the cost caused by later