The application discloses a rotor
system similarity test model design method considering gravity acceleration
distortion, and the method comprises the following steps: determining the similarity parameters of a
substructure on a target rotor
system according to a preset similarity relationship, wherein the preset similarity relationship comprises the similarity relationship of the
mass of a rotating shaft, the
mass of a
rotating disc and the
mass of a supporting structure, the similarity relationship of the polar
moment of inertia of the rotating shaft and the polar
moment of inertia of the
rotating disc, and the
substructure comprises the rotating shaft, the
rotating disc and the supporting structure; calculating experimental parameters based on the similarity parameters and actual parameters of the target rotor
system; and establishing a
similarity test model corresponding to the target rotor system based on the experimental parameters. The rotor system is divided into three substructures of the rotating shaft, the rotating disc and the supporting structure, and it is proposed that the similarity of the substructures can guarantee the similarity of the entire rotor system, the obtained
similarity test model guarantees that the inherent frequency and the
vibration response are completely consistent with the target rotor system while the size is reduced, and the cost, period and risk of the
similarity model experiment can be further reduced.