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Research on the cavitation in the pilot stage of flapper-nozzle hydraulic servovalve with fluid-structure interaction

机译:液固耦合的挡板式喷嘴液压伺服阀的空化研究。

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The fluid-solid interaction phenomenon in the pilot stage of flapper-nozzle servo valve and armature assembly structural stress field is the main reason of self-excited noise and instability. The cavitation phenomenon is the main source of servo valve noise and cavitation erosion. In order to study the mechanism of transient cavitation in the pilot stage of flapper-nozzle servo valve, the three-dimensional model, ICEM CFD software was used for meshing, star-ccm+ simulation software was used to simulate the cavitation and flapper movement characteristics in the flow field under the pilot stage fluid-structure interaction dynamic characteristics of the servo valve. The results show that the fluid-solid interaction of the flow field in the flapper-nozzle pilot valve can cause the periodic change of cavitation in the flow field, and the increase of inlet pressure at the nozzle and the movement of the flapper will aggravate the cavitation phenomenon. The conclusions in this paper can provide theoretical basis for the stability of servo valve and the prevention of cavitation.
机译:挡板喷嘴伺服阀的先导阶段与电枢组件的结构应力场发生流固耦合现象是产生自激噪声和不稳定的主要原因。空化现象是伺服阀噪声和空化腐蚀的主要来源。为了研究舌状喷嘴伺服阀的过渡阶段的空化机理,采用三维模型,使用ICEM CFD软件进行网格划分,使用star-ccm +仿真软件来模拟气门和挡板运动的特性。伺服阀在先导级流固耦合作用下的流场结果表明,挡板-喷嘴导向阀中流场的流固相互作用会引起流场中的空化的周期性变化,喷嘴入口压力的增大和挡板的运动会加重阀的流动。空化现象。本文的结论可为伺服阀的稳定性和防止气蚀提供理论依据。

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