Authors: Ke Ke Shi, Shuai Wang, Wan Jun Dou, Yan Yan Meng, Cui Li Chen, Bin Kun Ni
Abstract: Based on the current processing technology of large-scale spherical roller bearing rings, the dimensional expansion and contraction and the geometric variation of large-scale spherical roller bearing rings before and after heat treatment have been studied through several groups of processing experiment and data analysis. Optimization design of grinding allowance of large-scale spherical roller bearing rings have been implemented by using calculation formula of grinding allowance in bearing industry, which improved the production efficiency of the large spherical roller bearing rings and saved the manufacturing cost.
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Authors: Cao Hung Phi, Nguyen Thai Van, Le Hong Ky
Abstract: This paper presents a complete case study for designing and manufacturing chain parts for chain conveyor use for a harvest shallot for a real. The process of harvesting shallot in Vietnam is being done manually. Mechanization, automation of the harvest process has been demanded by farmers. In the harvest shallot equipment, the chain conveyor system is used to handling the desired orbit to the packing position. Shallots are uneven in size, distributed in a certain size range. Chain conveyor systems with the chain was non-standardized were choiced. Therefore, a complete design is required to meet requirement. The design procedures are: (1) calculation of the expected loads that exert on the chain during operation, (2) selection of materials, (3) designing the different parts of the chain taking into account safety, assembly process and economic considerations. The final design was justified and validated. The chain of chain conveyor system is working properly and safety under real conditions.
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Authors: Xin Yu Li, Chun Dong Zhu, Yan Chang Zhu
Abstract: Front cover is an important part of the car timing system, it is also an important parts of the engine to ensure the smooth flow.The quality of end cap is directly related to the normal and efficient operation of the engine.In this paper, through the research of the fine blanking process of the front cover of the timing system, a new type of fine blanking die is designed to improve the service life of the die and its parts.The influence rules of the process parameters such as the back top force, the counter pressure and the corner radius on punching smooth zone and the life of the mold, are analyzed by using the finite element software and a series of optimized process parameters are obtained after this.
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Authors: Wei Zhang, Chao Yan
Abstract: A method of optimization design of input location parameters is proposed to analyze this problem that stress suffered by arms is big in the lifting process of Scissor Lift Mechanism. On the basis of the established stress model, and through the analysis of maximum stress function in lifting process of SLM, the input location parameters are optimized. Finally, this conclusion and the feasibility of this scheme are validated by analysis of examples.
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Abstract: In this paper, finite element method was used to carry out parameter optimization and structural improvements of CNC machine. Considering the static and dynamic characteristics of the machine, the headstock and bed of CNC machine has been improved by structural optimizationk, and wall ribs was designed on the headstock CNC machine tools. After optimized the static stiffness and strength of CNC machine can meet the requirements, with a decrease of approximately 24.8% in weight compared to the original machine design.
605
Authors: Jie Shao, Zhi Qiang Li, Hui Yuan Xu, Xiu Quan Han, Rong Xia Zhang
Abstract: CAD models were built for a three-layer SPF/DB cylinder component. FEM method was employed to simulate the SPF/DB process with different girder structure at appropriate temperature/strain rate combinations. The results show that topology parameters of the structure influence the thickness of outer sheet and surface quality. When the thickness ratio of outer sheet to inner sheet exceeded 3:1 and the angle between adjacent ribs was great than 110 degree, ribs were formed and the cylinder surface was perfect. The simulation result was verified by experiment. The experimental results showed that the optimized cylinder structure can be formed at 920°C, 1×10-4 strain rate perfectly, and the size of blank cylinder diameter can be controlled accurately by SPF/DB mold and the size deviation is less than 0.5mm.
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Authors: Wei Jin, Bin Jie Mou, Hu Huang, Huan Bing Fu
Abstract: Stiffened Thin Wall Panel Structure is a widely used structural configuration in the design of aircraft’s inlet duct and large open bay. Vibration fatigue failure of stiffened panel structure will quickly emerges under strong broadband random loading environment which caused by shock waves moving at the inlet lip and cavity vortex and shear layer oscillation during flight. At present, a main research focus on dynamic strength design of aircraft’s light-weight structure is to reduce the dynamic stress response level in broadband random vibration environment ,so as to improve the ability of thin wall panel’s vibration fatigue property with light structure weight. Taking a stiffened thin panel of inlet duct as a typical case under random vibration excitation environment, an Advanced dynamical topology optimization methods is established based on the parametric modeling technique . Within the main frequency domain of external dynamic load, the maximum root mean square of stress (MRMSS) for global element of stiffened panel structure is calculated and optimized under the weight constraint with Genetic Optimization Algorithm (GOA). The comparison of structural stress response before and after optimization design shows that the maximum element RMS dynamic stress is reduced by 38% with the weight increased by about 9.8% and the purpose of improving vibration fatigue property is reached.
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Authors: Jun Liu, Pu Guo Gui, Jian Mei Wang, Yang Yu, Zheng Hu Zhong
Abstract: Frames are the main components of the flight motion simulator, which are the support for each shaft system, at the same time the rotating load for the external shaft, so the stiffness and dynamic characteristics of the frames in a large extent determines the final accuracy and dynamic performance of the flight motion simulator. For the cast aluminum alloy ZL114A frames of a 3-DOF flight motion simulator, using finite element analysis method, the dynamic characteristics are calculated and analyzed, and then the each order resonance frequency and mode of vibration are obtained. By using of the modal synthesis method and optimization algorithms, the structural dynamics of frames are designed optimally, so as to further reducing the moment of inertia, and improving the stiffness and dynamic characteristics of frames. This method has provided important reference for the reasonable design of the frame structure, and definitively established the foundation to further study the triaxial coupling dynamic characteristics and system mechanical optimization for the flight motion simulator.
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Authors: Xi Zhang, Xue Wu Dong, Dai Ren, Yan Ting Wang, Jian Hui Han, Yan Yan Yang
Abstract: This article studies optimization design of Vibratory stress relief (VSR) technology parameter for large welded components. The test is carried through a large welded truss. It first analysis key factor of the influence on VSR technology effect. And then by modal analysis, we’ve got the natural frequency and natural modes of the specimen , The optimization design is based on residual stress distribution and natural modes of component for VSR process parameters. Test pieces are treated by vibration. before and after vibration, residual stress of the specimens is measured by the method of blind hole.The results showed that vibration mode is a key factor in determining the effect of VSR. Stress distribution is more complex for large welded components.As accordance by selecting a few of vibration modes, for VSR main technical parameters design, it can get enough vibration displacement in the areas and directions of component with residual stress. Thus we can have a good effects to relief welding residual stress.Three major parameters (Excitation frequency, excitation point, support points) are related with vibration mode. They are decided by selecting vibration mode. Excitation force is decided based excitation frequency as well as the size of the exciter eccentric , to get the right excitation force by adjusting the size of the exciter eccentric under the condition of the selected excitation frequency.
1281
Authors: K.Z. Sun, J.Y. Zhou
Abstract: Analysis has been made on the adaptive optimization design of machining center tool changing manipulator by the application of the quantitative analysis tools. Thus adaptive comprehensive evaluation index is proposed and the adaptive comprehensive evaluation model of product is established. On the basis of primary evaluation on various indicators such as Product function adaptability with methods of Multilevel Fuzzy Integrative Evaluation, then, the secondary comprehensive evaluation will be continued and comprehensive adaptability evaluation level of FV-1100A machining center tool changing manipulator will be gained, thus providing guides and evidence for further improvement of product design. Through presenting adaptive measuring values of all proposals in schematic design phase and the quantitate evaluation on the complexity of modifying the design.
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