Research on design and verification methods of electric pump shock mount in civil aircraft hydraulic system

In this paper, the electric pump shock mount in civil aircraft hydraulic system is taken as the research object, and the design requirements, function realization and verification methods of the shock mount were comprehensively analyzed. At the same time, typical electric pump shock mounts were taken as an example to research and verify the design and verification methods. The results show that the shock mount has a good damping effect and can basically meet the damping requirements. The design and verification methods of the shock mount is reasonable and feasible, and can guide the design and verification of related products.