液壓缸試驗臺加載平臺的有限元分析
[Abstract]:The loading platform is an important part of the hydraulic cylinder test bench, and the platform and the pulley mechanism are two important parts of the loading platform. In this paper, a series of finite element structural analysis is carried out on the platform and the key parts in the pulley. The overall structure of the platform is composed of the left stand, the left center stand, the right stand, the support and the middle support. The bench is mainly used to load and install load cylinder and pulley parts, its structure and mechanical condition are complex. The pulley is mainly composed of the pulley frame, pull pressure sensor, pin shaft and other parts. It enables the test cylinder and the loading cylinder to smoothly connect the top through the pull pressure sensor. Due to the large stress of loading platform in the process of hydraulic cylinder test, the fatigue failure of the pulley can not be avoided, and then the enterprise suffers great losses in production and test. Therefore, it is very important to design the key components of the pulley and the bench, and it is also of practical significance to improve the reliability and service life of the loading platform. At the request of a hydraulic cylinder manufacturer, this paper analyzes the finite element structure of the key parts of the loading platform, such as the bench and the pulley. The structural characteristics of the loading platform are analyzed. Firstly, Pro/E software is used to model the platform and the pulley, and the interface technology between the software is used to achieve data sharing. According to the theory of finite element discretization, the finite element model is established in turn, the mesh is divided, the boundary condition is applied and the load is defined. Finally, the analysis results are obtained by calculation. According to the results obtained, the structural strength of the key parts in the bench and the pulley is checked by the strength theory, not only the distribution of stress and strain is obtained, but also the region of failure is clearly determined. When the maximum stress of the platform and the pulley is far lower than the allowable stress of the material and fully meets the requirements of the strength, the thickness of the bench and the pulley is reduced appropriately, so as to save the material and reduce the weight of the fuselage. The causes of fatigue failure are analyzed to ensure the rationality and reliability of the design. This method improves the efficiency of loading platform design and reduces the cost of loading platform design and manufacturing. It is worth mentioning that the actual working conditions are in good agreement with the finite element analysis results in this paper. Therefore, this paper is objective and credible in theoretical analysis, and has certain guiding significance to the actual test and production process.
【學(xué)位授予單位】:沈陽工業(yè)大學(xué)
【學(xué)位級別】:碩士
【學(xué)位授予年份】:2012
【分類號】:TH137.51
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