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Research on cavitation phenomena in pilot stage of jet pipe servo-valve with a rectangular nozzle based on large-eddy simulations

机译:基于大涡模拟矩形喷嘴的喷射管伺服阀试验阶段空化现象研究

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摘要

The flow field in the pilot stage of a jet pipe servo-valve significantly affects the performance of the valve. Cavitation with pressure oscillations occur in the pilot stage and lead to the appearance of high-frequency noise and vibration. To obtain dynamic characteristics of cavitation and study the relationship between the cavitation and inlet pressure, we use large-eddy simulations (LESs) to calculate the unsteady flow field in the pilot stage with a rectangular nozzle. The simulation results show that fixed cavitation and vortex cavitation exist, and travelling cavitation begins to occur when inlet pressure reaches 7MPa. The increment of inlet pressure enhances cavitation and cavitation shedding. The cavitation-shedding process under different inlet pressures is monitored via LES. Different points are studied, which differ in terms of cavitation type and the development of cavitation regions. By applying a fast Fourier transform, we obtain the main frequencies of the pressure oscillations of each cavitation under different inlet pressures. The influences of outlet pressure and wedge length are also studied. When outlet pressure and wedge length increase, cavitation phenomena are weakened effectively. When the wedge length increases, the main frequency of vortex cavitation increases whereas that of travelling cavitation decreases. Upon increasing the wedge length, the volume fraction of vapor phase and the energy ratio at the surface at y= −0.3mm to the exit of the nozzle decrease, and both decrease sharply from 0.03 to 0.04mm. Considering the above characteristics and the ease of the process, the optimal length of the wedge is 0.03mm.
机译:喷气管伺服阀的试验台中的流场显着影响阀门的性能。具有压力振荡的空化发生在试验台中,导致高频噪声和振动的外观。为了获得空化的动态特性并研究空化和入口压力之间的关系,我们使用大涡模拟(较少)用矩形喷嘴计算导频阶段的非定常流场。仿真结果表明,存在固定空化和涡旋空心,当入口压力达到7MPa时,行驶空间开始发生。入口压力的增量增强了空化和空化脱落。通过LES监测不同入口压力下的空化脱落过程。研究了不同的点,这在空化型和空化区域的发展方面不同。通过应用快速傅里叶变换,我们在不同的入口压力下获得每个空化的压力振荡的主频率。还研究了出口压力和楔形长度的影响。当出口压力和楔形长度增加时,有效地减弱了空化现象。当楔形长度增加时,涡流空化的主频率增加,而行驶空化的主要频率降低。在增加楔形长度时,蒸汽相的体积分数和在y = -0.3mm处的表面处的能量比下降到喷嘴的出口,并且两者从0.03到0.04mm的急剧下降。考虑到上述特性和易于过程,楔形的最佳长度为0.03mm。

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