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201.
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徐家文%朱永伟%胡平旺%云乃彰%严德荣 《宇航材料工艺》2003,33(1):13-17
综述了整体叶轮的主要加工方法及其比较,就数控展成电解加工的重要技术特点(可以综合发挥数控技术和电解加工两者的技术优点)进行了论述,展示了数控电解在加工整体叶轮、解决以数控铣、精密铸造难加工或不能加工的技术难题方面所显示的优越性。该项工艺技术对于新型航天发动机的研制具有重要意义和广阔的应用前景。 相似文献
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分析了柔性铰链及压电陶瓷的原理和特点,指出了压电陶瓷-柔性铰链机构在微进给中具有高响应频率、高精度和无间隙等优点,满足微细电火花加工的要求。并将压电陶瓷与整体式柔性铰链相结合,设计出一种压电驱动蠕动式微进给机构。 相似文献
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离心轮水力性能的优劣对泵的效率影响最大,离心轮加工质量好坏直接影响泵的特性。针对钎焊式离心轮加工的技术要求与技术难点进行分析、研究,结合现有数控设备对离心轮的加工工艺进行改进、优化及数控加工转化。 相似文献
207.
This article presents a mathematical model of helical end-milling forces through experimental identification of the cutting coefficients and analyzes the changes of corner-milling forces under different conditions. In allusion to the corner-milling process, the relationship between working parameters and the corner coordinates is investigated by way of combination of tool tracing and cutting geometrodynamics. The milling parameters are optimized by changing the coordinates of tool center and working parameters without altering cutting forces. By applying the optimized parameters to milling practice, a comparison is made to show the improved product quality. Based on these optimized parameters, a finite element method (FEM) program is used to compute deformation values of a workpiece's corner, which evidences few effects that optimized parameters can exert on the corner deformation. 相似文献
208.
Oriented to CAD/CAM seamless integration, this paper presents an idea for synthetically considering the qualitative history model, which represents the whole course of modeling, and the quantitative geometry model, which contains the extended Brep model, CSG and feature pedigree. History model building captures in background the dynamic interactive definition of engineering requirement and then explicitly conveys the original intention to successive application layers, which isc onductive to the decision support of manufacturing planning in not only automatic geometry re-constructing but also machining set-up. G-DSG theory as an earlier achievement is applied to generate the topology-independent generalized mid-model as an input to manufacturing planning, which istherefore simplified and its accuracy is simultaneously improved. Manufacturing planning lays emphasis on optimizing the mapping in both geometry and function from part itself to detail machining scheme. Comparatively, process planning pays more attention to the mapping to those items like tool, fixture, etc. Theoretically, such an idea is also beneficial to realizing the parametric NC machining trajectory generation and maintaining its dynamic consistency with the update of the design model. 相似文献
209.
The problem of finished surface being not first-order continuous commonly exists in machining sculptured surfaces with a torus cutter and some other types of cutters. To solve this problem, a dual drive curve tool path planning method is proposed in this article. First, the maximum machining strip width of a whole tool path can be obtained through optimizing each tool position with multi-point machining (MPM) method. Second, two drive curves are then determined according to the obtained maximum machining strip width. Finally, the tool is positioned once more along the dual drive curve under the condition of tool path smoothness. A computer simulation and cutting experiments are carried out to testify the performance of the new method. The machined surface is measured with a coordinate measuring machine (CMM) to examine the machining quality. The results obtained show that this method can effectively eliminate sharp scallops between adjacent tool paths, keep tool paths smooth, and improve the surface machining quality as well as machining efficiency. 相似文献
210.
针对农用无人机超低空表型遥感和喷药精准悬停易受地效扰动问题,提出了一种自适应ADRC姿态控制器。首先设计了基于ADRC的姿态控制器,结合四旋翼无人机平台在0.9~1.1、1.1~1.3、1.4~1.6、2.0~2.4、2.5~2.9、3.3~3.6 m/s侧向水平风、0.9~1.1 m/s (11°)、1.1~1.3 m/s (13°)、1.4~1.6 m/s (18°)、1.8~2.0 m/s (18°)、2.1~2.5 m/s (18°)前俯向风和侧俯向风下进行干扰的预测和控制量的补偿实验。实验结果显示使用ADRC姿态控制器后无人机抗风性能有较大提升。然而在存在初始误差时,ADRC固定带宽无法满足要求,进一步设计了自适应ADRC姿态控制器(ILC-ADRC)。通过迭代学习控制在线优化自抗扰控制器带宽,实现了不同增益观测器的自适应整定。实验结合四旋翼无人机平台分别进行了机头实际方向与期望方向偏离55°、90°、180°,水平风速1.1~1.3、1.4~1.6、2.0~2.4、2.5~2.9 m/s下使用ADRC和ILC-ADRC的对比。实验结果显示采用ILC-ADRC姿态控制器,在150次控制周期内,偏航角误差均在-15°~15°之间,满足四旋翼无人机偏航角控制精度要求,同时调节时间分别缩短了40%,16.67%,12.5%,53.33%,10.34%,13.95%,27.27%,58.66%,11.86%。 相似文献