确定节流孔直径对惯性流体力学装置流体流动的影响

B. Nussupbekov, M. S. Ovcharov, E. Z. Oshanov, U. B. Yesbergenov, M. Duisenbayeva, A. A. Tishbekov, M. K. Amanzholova
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引用次数: 0

摘要

为了解决与建筑物和构筑物供暖有关的环境问题,文章考虑了将电能转化为热能的方法以及同时发生的过程。众所周知的热能设备,如涡流、空化、空化-涡流、旋转等,并不能完全满足消费者的要求。在这种情况下,寻找有效的解决方案成为当务之急。这些解决方案包括通过旋转液体的惯性力在节流阀开口处产生压力来获取热能的方法。为了确定流经节流孔的液体流量,我们制作了一个实验台。借助支架,我们测定了液体通过直径为 1.5、2、3 毫米的节流孔的流量。实验发现,节流孔直径越大,液体流量越大。但是,节流孔的直径不能过分增大,否则会使节流孔处产生的压力复杂化。研究发现,随着转子角速度的增大,节流阀开口处的流体压力会增大,总流量中来自初静压的流体流量比例会减小。可以肯定的是,只有在转子速度较低(ω = 76 rad / s 以下)时,供油管中的初静压才会对流量产生显著影响,而随着角速度的增加,其影响会减小,系数 k 趋于 1。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Determination of the effects of the diameters of the throttle holes on the fluid flow of an inertial hydrodynamic installation
In the article, in order to solve environmental problems associated with heating buildings and structures, the methods of converting electrical energy into thermal energy and the processes occurring at the same time are considered. Well-known thermal installations, such as vortex, cavitation, cavitation-vortex, rotary, do not fully meet the requirements of consumers. In these conditions, the search for effective solutions is an urgent task. Such solutions include a method of obtaining thermal energy by creating pressure at the throttle openings by inertia forces of a rotating mass of liquid. To determine the flow of liquid through the throttle holes, an experimental stand was made. With the help of the stand, we determined the flow rate of liquid through throttle holes with a diameter of 1.5, 2, 3 mm. During the experiment, it was found that the larger the diameter of the throttle opening, the higher the fluid flow. However, it is impossible to excessively increase the diameter of the throttle opening, as this will complicate the creation of pressure at the throttle openings. It is found that with an increase in the angular velocity of the rotor, the fluid pressure at the throttle openings increases, and the proportion of fluid flow from the preliminary static pressure in the total flow decreases. It is certain that the preliminary static pressure in the supply line has a significant effect on the flow rate only at low rotor speeds (ω up to = 76 rad / s), and with increasing angular velocity, its influence decreases and the coefficient k tends to 1.
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