摘要
The methods for reducing interface aperture inconsistency are studied in NC orbital milling(NCOM)of CFRP/Ti6Al4V laminates with coarse pitch.Comparative experiments show burr,aperture inconsistency and error are typical interface defects.Meanwhile,aperture inconsistency and error are more serious than burr in NCOM with coarse pitch.As one of the major causes of interface defects,axial force and radial force are intensively studied.Based upon the machining principle of orbital milling(OM)and the actual hole-making condition in laminated structures,NCOM experiments with coarse pitch are conducted on CFRP/Ti6Al4V laminates under different cutting conditions.Then,the effects of interlayer clamping,minimal quantity lubrication(MQL),twice milling instead of reaming,and interlayer speed change on interface aperture are analyzed.Research shows that interlayer clamping,interlayer speed change and MQL can effectively reduce out-of-tolerance of interface aperture.When making holes of different diameters with one cutter,axial feed has a greater effect on interface aperture precision than tangential feed.When making holes of the same diameter with different cutters,small diameter cutter will reduce interface aperture precision in a single processing.But the method of“twice milling instead of reaming”can improve the aperture precision effectively.
研究了大螺距数控螺旋铣削(NC orbital milling,NCOM)飞机叠层结构界面孔径非一致性缺陷的抑制方法。对比试验表明,毛刺、孔检非一致性和误差是典型的界面缺陷,其中大螺距螺旋铣削制孔时孔径非一致性和误差比毛刺更为严重。作为影响界面缺陷的主要因素,对轴向力和径向力进行了深入研究。从螺旋铣孔(Orbital milling,OM)的加工机理和叠层制孔的实际工况出发,对CFRP/Ti6Al4V叠层结构进行了不同切削条件下大螺距NCOM制孔试验,分析了叠层夹紧、切削参数、微量润滑(Minimal quantity lubrication,MQL)、以铣代铰、层间变速等方法对界面孔径的影响。研究结果表明,层间夹紧、层间变速及MQL均可有效抑制界面孔径对接超差缺陷。当采用一把刀具加工不同尺寸孔径时,轴向进给对界面孔径精度的影响比切向进给显著;当采用多把不同加工同一尺寸孔径时,小直径刀具会降低一次加工时界面孔径精度,但可以采取"二次以铣代铰"方法改善孔径加工精度。
基金
Natural Science Research in Jiangsu Province(No.17KJB460008)
the 333 Project Research Funding Project in Jiangsu Province(No.BRA2018310)
the Innovation Project of Jiangsu Province.
