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Indeterminate mechanics model for bearing capacity of constant flow oil pocket in hydrostatic slide

机译:静水滑道恒流油穴承载力的不确定力学模型

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With the development of aviation industry, higher requirements are placed on the reliability and precision of aerospace components. Hydrostatic bearing technology is widely used in the aviation field. In this paper, the static pressure guide rail is taken as an example to study the calculation method of the bearing capacity of the static pressure bearing cavity, so as to obtain more accurate oil cavity bearing capacity, and then prepare for improving the reliability and precision of researching aerospace components. At present, the method called 'Translating External Load' is generally used to analyze the bearing capacity of the oil pocket. Since the mechanics model of 'Translating External Load' method varies with the variation arrangement of the oil pocket, so 'Translating External Load' method has less commonality. According to the principle of superposition of force and the idea of converse thinking, the bearing capacity of the oil pocket with constant flow supply is divided into six parts, each part bearing the component of external load, and the mechanics model can be established. Based on the mechanics model built, the equation of the bearing capacity of each oil pocket can be derived with each load component acting on the hydrostatic slide. When the arrangement of the oil pocket is complicated, the computation of bearing capacity turns into the problem of statically indeterminate. Referring to the solution method of 'Elastic Body', the compatibility equations of deformations of oil film are presented, the statically indeterminate problem is translated into statically determinate problem, and the bearing capacity of each oil pocket is obtained. Vector superposition is carried to the six bearing capacity components of each oil pocket, and then the final equations calculating the bearing capacity of the oil pocket can be attained. The research work offers the general method for calculating the bearing capacity of the oil pocket, and the equations can be solved with the help of the computer programs and can improve the design efficiency and accuracy.
机译:随着航空工业的发展,对航空航天部件的可靠性和精度提出了更高的要求。静压轴承技术被广泛应用于航空领域。本文以静压导轨为例,研究静压轴承腔承载力的计算方法,以获得更准确的油腔承载力,为提高可靠性和精度做准备。研究航空航天部件。目前,通常使用称为“转换外部载荷”的方法来分析油囊的承载能力。由于“平移外部载荷”方法的力学模型会随着油穴的变化而变化,因此“平移外部载荷”方法的通用性较低。根据力的叠加原理和逆向思维的思想,将恒定供油量的油穴的承载能力分为六个部分,每个部分承担外力分量,建立力学模型。根据建立的力学模型,可以推导出每个油穴的承载力方程,其中每个载荷分量都作用在静液压滑块上。当油囊的布置复杂时,承载力的计算就变成了静态不确定的问题。参照“弹性体”的求解方法,给出了油膜变形的相容方程,将静定问题转化为静定问题,得到了每个油穴的承载力。将矢量叠加传递到每个油腔的六个承载能力分量,然后可以得出计算油腔的承载能力的最终方程式。研究工作提供了计算油穴承载力的通用方法,该方程可以借助计算机程序求解,可以提高设计效率和精度。

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