Abstract
Abstract Double-span rotor systems are commonly used in aerospace engines and large turbines, where critical criticality is critical in their dynamic characteristics. This paper calculates the critical critical value of the rotor through the intervention matrix method and verifies it through the finite element method. The changes in the support and wheel disc were discussed and the results show that the increase in support stiffness, the reduction in wheel disc mass, and the increase in coupling stiffness will increase the critical stress of the double-span rotor. In addition, the increase in the position of the support and the installation position of the coupling will affect the critical point.
Published Version
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