School of Mechanical Engineering, Yanshan University, Qinhuangdao 066004, China.
School of Naval Architecture and Ocean Engineering, Jiangsu Maritime Institute, Nanjing 211199, China.
Sensors (Basel). 2022 Dec 25;23(1):216. doi: 10.3390/s23010216.
Jet pipe servo-valves are widely used in high-precision servo control systems. However, the accuracy of pressure-flow characteristic equations relevant to its pilot stage needs to be improved. In contrast to the traditional analytical approach using the orifice equation, the article investigates the pressure and flow characteristics of the pilot stage based on the impact jet principle. Taking the pre-stage of a certain type of jet pipe servo-valve as an example, the flow field is simulated using ANASYS software. By comparing the simulation data with the calculation results, the pressure characteristic model is basically consistent with the simulation data, and the relative error is less than 2.3%. The error between the revised flow characteristic model and the simulation result is small, and the maximum deviation is less than 0.0022 L/min. Finally, to verify the applicability of the model to other specifications, the experimental data in the literature are compared with the theoretical calculation results, the maximum relative error of pressure characteristics is 2.19%, and the relative error of flow characteristics is less than 5.34%.
射流管伺服阀在高精度伺服控制系统中得到了广泛的应用。然而,其先导级相关的压力-流量特性方程的精度需要进一步提高。与传统的基于孔口方程的解析方法相比,本文基于冲击射流原理研究了先导级的压力和流量特性。以某型射流管伺服阀的前置级为例,利用 ANASYS 软件对其流场进行了模拟。通过将仿真数据与计算结果进行对比,压力特性模型与仿真数据基本吻合,相对误差小于 2.3%。修正后的流量特性模型与仿真结果的误差较小,最大偏差小于 0.0022 L/min。最后,为了验证模型对其他规格的适用性,将文献中的实验数据与理论计算结果进行了对比,压力特性的最大相对误差为 2.19%,流量特性的相对误差小于 5.34%。