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An automated approach to calculating the maximum diameters of multiple cutters and their paths for sectional milling of centrifugal impellers on a 4_(1/2)-axis CNC machine 被引量:5
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作者 Baohai WU Zezhong C.CHEN +2 位作者 Ming LUO Dinghua ZHANG Feiyan HAN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第4期1030-1039,共10页
Power generators and chemical engineering compressors include heavy and large centrifugal impellers. To produce these impellers in high-speed machining, a 4?-axis milling machine(or a 4-axis machine plus an indexing t... Power generators and chemical engineering compressors include heavy and large centrifugal impellers. To produce these impellers in high-speed machining, a 4?-axis milling machine(or a 4-axis machine plus an indexing table) is often used in the industry, which is more rigid than a5-axis milling machine. Since impeller blades are designed with complex B-spline surfaces and impeller channels spaces vary significantly, it is more efficient to use multiple cutters as large as possible to cut a channel in sections and a blade surface in patches, instead of only using a small cutter to machine a whole blade and a channel. Unfortunately, no approach has been established to automatically calculate the largest diameters of cutters and their paths, which include the indexing table angles. To address this problem, an automated and optimization approach is proposed. Based on the structure of a 4?-axis machine, a geometric model for a cutter gouging/interfering the impeller is formulated, and an optimization model of the cutter diameter in terms of the indexing table angle is established at a cutter contact(CC) point on a blade surface. Then, the diameters of the tools,their orientations, and the indexing table angles are optimized, and each tool's paths are generated for machining its corresponding impeller section. As a test, an impeller is efficiently machined with these tools section by section; thus, this approach is valid. It can be directly used in the industry to improve efficiency of machining centrifugal impellers. 展开更多
关键词 Automated path generation 4_(1/2)-axis CNC machining Centrifugal impeller machining Cutter diameter optimization Sectional machining
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超大幅面全固态Nd:YAG激光标刻机的研制 被引量:2
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作者 王菲 李伟 +2 位作者 闫钰峰 李凯 麻宏宇 《长春理工大学学报(自然科学版)》 2008年第4期68-70,67,共4页
研制了一台超大幅面全固态激光标刻机,该系统主要由光纤耦合输出的全固态激光器、两轴联动工作台和控制系统等组成,详细介绍了两轴联动工作台的设计及其控制系统。通过高精度机械传动部件实现激光束与工件的相对运动,由传能光纤输出的... 研制了一台超大幅面全固态激光标刻机,该系统主要由光纤耦合输出的全固态激光器、两轴联动工作台和控制系统等组成,详细介绍了两轴联动工作台的设计及其控制系统。通过高精度机械传动部件实现激光束与工件的相对运动,由传能光纤输出的高能量激光对工件进行标刻,不仅可以实现大范围、高精度标刻,而且输出激光稳定、能量转换效率较高,能够实现高质量的标刻。 展开更多
关键词 激光标刻 全固态Nd:YAG激光器 两轴联动工作台
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Lateral aerodynamic performance and speed limits of double-deck container vehicles with different structures 被引量:2
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作者 李燕飞 田红旗 《Journal of Central South University》 SCIE EI CAS 2012年第7期2061-2066,共6页
Based on 3D, steady N-S equations and k-e turbulence model, Fluent was employed to do numerical simulation for lateral aerodynamic performance of 6-axis X2K double-deck container trains with two different loading form... Based on 3D, steady N-S equations and k-e turbulence model, Fluent was employed to do numerical simulation for lateral aerodynamic performance of 6-axis X2K double-deck container trains with two different loading forms, and speed limits of the freight trains were studied. The result indicates that under wind environment: 1) As for vehicles without and with cross-loaded structure, aero-pressure on the former is bigger, but air velocity around the latter is larger; 2) When sideslip angle θ=0°, the airflow is symmetry about train vertical axis; when θ〉0°, the airflow is detached at the top of vehicles, and the air velocity increases above the separated line but decreases below it; 3) With θ increasing, the lateral force on the mid vehicle firstly increases but decreases as θ=75°; 4) When the 6-axis X2K fiat car loads empty boxes of a 40 ft and a 48 ft at 120 km/h, the overturning wind speed is 25.19 m/s, and the train should be stopped under the 12th grade wind speed. 展开更多
关键词 numerical simulation 6-axis X2K flat car loading form lateral aerodynamic performance speed limit
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