北京航空航天大学机械工程与自动化学院,北京,100191
纸质出版:2020
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李东升,游佳琪,王明明. 蜂窝夹层结构高精度面板的三维铣削研究[J]. 航空制造技术, 2020, 63(9): 74-82.
LI Dongsheng, YOU Jiaqi, WANG Mingming. Research on 3D Milling of Honeycomb Sandwich Structure High-Precision Panel. Aeronautical Manufacturing Technology, 2020, 63(9): 74-82.
李东升,游佳琪,王明明. 蜂窝夹层结构高精度面板的三维铣削研究[J]. 航空制造技术, 2020, 63(9): 74-82. DOI: 10.16080/j.issn1671-833x.2020.09.074.
LI Dongsheng, YOU Jiaqi, WANG Mingming. Research on 3D Milling of Honeycomb Sandwich Structure High-Precision Panel. Aeronautical Manufacturing Technology, 2020, 63(9): 74-82. DOI: 10.16080/j.issn1671-833x.2020.09.074.
建立了蜂窝夹层结构高精度面板三维铣削有限元仿真模型,分析了主轴转速、进给速度、铣削深度等因素对铣削后面板表面粗糙度及温度的影响规律,进行了蜂窝夹层结构面板的正交铣削试验及水超声脉冲反射法无损检测试验,优化了铣削加工参数;在面板铣削仿真和试验分析的基础上,以最优加工参数设计了焦距分别为 5500mm、 2750mm、1090mm 的 400mm×400mm 双曲率夹层结构高精度面板的铣削精加工试验及超声波脉冲穿透法无损检测试验,测量了面板铣削前后的型面精度及表面粗糙度。结果表明:模拟与试验结论一致;铣削后面板表面粗糙度与主轴转速负相关,与铣削深度和进给速度正相关;面板温度主要由铣削深度决定,单次铣削深度超过 300μm 时,面板温度超过环氧树脂胶的玻璃态转变温度(313K),夹层结构发生轻微脱粘;铣削后的双曲率面板型面精度数值、峰峰值(波峰 – 波谷值)及表面粗糙度数值均显著降低,且无脱粘现象,验证了铣削工艺在保证结构稳定性的基础上可提高面板表面质量。
The 3D milling finite element simulation model of honeycomb sandwich structure high-precision panel is established. The influence of the spindle speed
the feed speed and the milling depth on the surface roughness and the temperature of the honeycomb sandwich panel are analyzed. The orthogonal milling experiment and non-destructive testing of water ultrasonic pulse reflection method have been carried out
in company with optimizing the milling parameters. Based on the simulation analysis and experiment
the 400mm×400mm double-curvature high-precision sandwich panels with focal lengths of 5500mm
2750mm
and 1090mm are milled
as well as non-destructive testing of ultrasonic pulse penetration method. Meanwhile both the surface precision and roughness are inspected before and after forming. The results show that the experimental results are consistent with the finite element simulation. The surface roughness of the sandwich plate after milling is negatively correlated with the spindle speed
and is positively correlated with the milling depth and feed rate. Plus
the panel temperature is mainly determined by the milling depth. When the single milling depth exceeds 300μm
the panel temperature exceeds the glass transition temperature of the epoxy resin (313K)
and the sandwich structure is slightly debonded. Eventually the precision value
the peak-to-peak value (crest-to-valley value) and the surface roughness value of the double-curvature panels are significantly reduced. No debonding phenomenon occurs simultaneously. It is verified that milling can improve the surface quality of the panel on the basis of ensuring structural stability.
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