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冰箱压缩机曲柄连杆机构振动分析 被引量:4
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作者 韩宝坤 纪瑶 +1 位作者 常羽宁 常胜 《山东科技大学学报(自然科学版)》 CAS 北大核心 2019年第4期100-106,共7页
压缩机曲柄连杆机构产生的不平衡惯性力是产生振动和噪声的根源。减小不平衡惯性力,是降低压缩机振动噪声的重要途径。建立了偏心式曲柄连杆结构的物理模型和数学模型,理论分析得出,平衡块质径积和曲轴偏置是影响惯性力的主要参数。建... 压缩机曲柄连杆机构产生的不平衡惯性力是产生振动和噪声的根源。减小不平衡惯性力,是降低压缩机振动噪声的重要途径。建立了偏心式曲柄连杆结构的物理模型和数学模型,理论分析得出,平衡块质径积和曲轴偏置是影响惯性力的主要参数。建立了制冷压缩机多体动力学模型,得到了加速度频响曲线,分析了平衡块质径积和曲轴偏置对振动的影响,给出了最佳取值范围,通过实验验证了仿真结果的正确性。采用多体动力学仿真与振动实验相结合的方法,为压缩机曲柄连杆机构的参数设计,降低压缩机振动噪声,提供了新的途径。 展开更多
关键词 曲柄连杆机构 平衡块 曲轴偏置 振动仿真分析 幅频响应 压缩机
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Launching and Travelling Dynamic Analysis of Rocket Launcher System ──The Study of a Unified Model
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作者 王春峰 宋廷伦 《Journal of Beijing Institute of Technology》 EI CAS 1995年第2期221+215-221,共8页
A unified model which is used to study the launching and travelling dynamic properties of a rlcket/launcher system is established. In this model, the rocket, the launcher,and the launching vehicle are considered as a... A unified model which is used to study the launching and travelling dynamic properties of a rlcket/launcher system is established. In this model, the rocket, the launcher,and the launching vehicle are considered as an interacting dynamic system in order to study the dynamic interaction between the various parts of the system and the optimal parameter matching among the above mentioned parts. The following random factors are taken into account in this paper. road surface excitation. rocket mass center misalignment, thrust misalignment, dynamic of the rocket, and the cross wind. Based on this unified model, a computer simulation software is developed, some simulation work has been carried out, and certain beneficial results have been achieved. 展开更多
关键词 simulation dispersion analysis/travelling vibration multiple rocket
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