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基于Pro/E的星型轮的三维参数化设计
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作者 徐年富 张志成 《中外企业家》 2017年第4期145-146,共2页
随着现代科学技术的高速发展,对机械传动机构的高速、高精度、高强度、高性能要求也越来越高。为了使产品性能达到这些高标准,就要求机器的传动部分在设计过程中要进行三维参数化设计,并动态模拟、仿真,但传动机构中的齿轮设计要求各不... 随着现代科学技术的高速发展,对机械传动机构的高速、高精度、高强度、高性能要求也越来越高。为了使产品性能达到这些高标准,就要求机器的传动部分在设计过程中要进行三维参数化设计,并动态模拟、仿真,但传动机构中的齿轮设计要求各不相同,有些齿轮的设计比较烦琐,如星型轮等,因此必须借助于功能强大的设计软件。基于此,利用Pro/E强大的设计软件系统,对星型轮进行三维参数化设计,可以简化设计过程,并为后期的装配、机构动态模拟、仿真操作、适时进行参数化修改带来方便。 展开更多
关键词 星型轮 三维参数化 设计 矿山 PRO/E
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PC生产线自动布料机研究
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作者 姚传富 《现代制造技术与装备》 2024年第3期212-214,共3页
混凝土预制件(Precast Concrete,PC)生产线是支撑建筑产业工业化和现代化发展的关键装备,布料机是PC生产线的核心设备,对生产线的自动化程度、可靠性、工作效率及构件质量有着决定性影响。通过研究自动布料机布料装置和控制系统,提供一... 混凝土预制件(Precast Concrete,PC)生产线是支撑建筑产业工业化和现代化发展的关键装备,布料机是PC生产线的核心设备,对生产线的自动化程度、可靠性、工作效率及构件质量有着决定性影响。通过研究自动布料机布料装置和控制系统,提供一种切实可行的自动布料解决方案,同时指出布料机未来的发展方向。 展开更多
关键词 混凝土预制件(PC)生产线 自动布料机 布料装置 控制系统 星型轮
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基于ADAMS的花生收获机清选装置设计与仿真研究 被引量:4
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作者 张莉 郭巧惠 徐嘉 《农机化研究》 北大核心 2017年第3期53-57,共5页
花生清选分离是花生收获机作业过程中最重要的项目之一,是收获机的核心部件,其性能的好坏直接关系到收获机的作业质量,其主要的指标是含杂率与损失破碎率。为了提高花生清选分离装置的设计效率、缩短设计周期,提出了一种基于ADAMS的花... 花生清选分离是花生收获机作业过程中最重要的项目之一,是收获机的核心部件,其性能的好坏直接关系到收获机的作业质量,其主要的指标是含杂率与损失破碎率。为了提高花生清选分离装置的设计效率、缩短设计周期,提出了一种基于ADAMS的花生收获机清选装置虚拟设计和仿真方法,并对核心部件做了重点设计,包括轮轴和星型轮。利用非自由质点坐标系和广义坐标系,结合拉格朗日方程的位置和速度约束,建立了清选装置的机械系统运动学微分方程。使用ADAMS软件对不同转速条件下的轮轴工作效果进行了动力学仿真,得到了3种不同速度下的Y轴速度曲线,通过比较曲线的震动效果,选择合适的轮轴转速,对花生收获机的优化设计具有重要的借鉴意义。 展开更多
关键词 花生收获机 清选装置 虚拟仿真 ADAMS软件 星型轮
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Bifurcation and chaos study on transverse-torsional coupled 2K-H planetary gear train with multiple clearances 被引量:4
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作者 盛冬平 朱如鹏 +2 位作者 靳广虎 陆凤霞 鲍和云 《Journal of Central South University》 SCIE EI CAS CSCD 2016年第1期86-101,共16页
A new non-linear transverse-torsional coupled model was proposed for 2K-H planetary gear train, and gear's geometric eccentricity error, comprehensive transmission error, time-varying meshing stiffness, sun-planet... A new non-linear transverse-torsional coupled model was proposed for 2K-H planetary gear train, and gear's geometric eccentricity error, comprehensive transmission error, time-varying meshing stiffness, sun-planet and planet-ring gear pair's backlashes and sun gear's bearing clearance were taken into consideration. The solution of differential governing equation of motion was solved by applying variable step-size Runge-Kutta numerical integration method. The system motion state was investigated systematically and qualitatively, and exhibited diverse characteristics of bifurcation and chaos as well as non-linear behavior under different bifurcation parameters including meshing frequency, sun-planet backlash, planet-ring backlash and sun gear's bearing clearance. Analysis results show that the increasing damping could suppress the region of chaotic motion and improve the system's stability significantly. The route of crisis to chaotic motion was observed under the bifurcation parameter of meshing frequency. However, the routes of period doubling and crisis to chaos were identified under the bifurcation parameter of sun-planet backlash; besides, several different types of routes to chaos were observed and coexisted under the bifurcation parameter of planet-ring backlash including period doubling, Hopf bifurcation, 3T-periodic channel and crisis. Additionally, planet-ring backlash generated a strong coupling effect to system's non-linear behavior while the sun gear's bearing clearance produced weak coupling effect. Finally, quasi-periodic motion could be found under all above–mentioned bifurcation parameters and closely associated with the 3T-periodic motion. 展开更多
关键词 planetary gear train BIFURCATION CHAOS transverse-torsional coupling BACKLASH bearing clearance
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Analysis of lubrication performance for internal meshing gear pair considering vibration 被引量:3
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作者 JIAN Guang-xiao WANG You-qiang +2 位作者 ZHANG Ping LI Yun-kai LUO Heng 《Journal of Central South University》 SCIE EI CAS CSCD 2021年第1期126-139,共14页
The thermal elasto-hydrodynamic lubrication characteristics of the internal meshing gears in a planetary gear train under vibrations were examined considering the influence of the modification coefficient and time-var... The thermal elasto-hydrodynamic lubrication characteristics of the internal meshing gears in a planetary gear train under vibrations were examined considering the influence of the modification coefficient and time-varying meshing stiffness.Based on dynamic theory of the gear system,a dynamic model of the planetary gear train was established.The lubrication performances of modified gear systems under vibrations and static loads were analyzed.Compared with other transmission types,the best lubrication effect could be produced by the positive transmission.A thicker lubricating oil film could be formed,and the friction coefficient and oil film flash temperature are the smallest.Increasing modification coefficient improves the lubrication performance continuously but intensifies the engage-in and tooth-change impact.For the planetary and inner gears,the increase in the modification coefficient also leads a decrease in the oil film stiffness. 展开更多
关键词 internal meshing gears dynamic model modification coefficient lubrication performance oil film stiffness
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Attitude stabilization of a pico-satellite by momentum wheel and magnetic coils 被引量:5
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作者 Tao MENG Hao WANG +1 位作者 Zhong-he JIN Ke HAN 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2009年第11期1617-1623,共7页
The three-axis active attitude control method with a momentum wheel and magnetic coils for a pico-satellite is considered. The designed satellite is a 2.5 kg class satellite stabilized to nadir pointing. The momentum ... The three-axis active attitude control method with a momentum wheel and magnetic coils for a pico-satellite is considered. The designed satellite is a 2.5 kg class satellite stabilized to nadir pointing. The momentum wheel performs a pitch-axis momentum bias, nominally spinning at a particular rate. Three magnetic coils are mounted perpendicularly along the body axis for precise attitude control through the switch control mechanism. Momentum wheel start up control, damping control and attitude acquisition control are considered. Simulation results show that the proposed combined control laws for the pico-satellite is reliable and has an appropriate accuracy under different separation conditions. The proposed strategy to start up the wheel after separation from the launch vehicle shows that its pitch momentum wheel can start up successfully to its nominal speed from rest, and the attitude convergence can be completed within several orbits, depending on separation conditions. 展开更多
关键词 Pico-satellite Attitude control Magnetic coils Momentum wheel
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