C/E复合材料“以磨代钻”制孔工艺  被引量:10

Drilling Process of C/E Composites With Grinding Tool

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作  者:鲍永杰[1] 高航[1] 董波[2] 李兰柱[2] 

机构地区:[1]大连理工大学精密与特种加工教育部重点实验室,大连116024 [2]航天材料及工艺研究所,北京100076

出  处:《宇航材料工艺》2010年第4期47-49,共3页Aerospace Materials & Technology

基  金:国家自然科学基金资助项目(50875034);国家863计划资助项目(SQ2008AA04XK1478912)

摘  要:为了提高C/E复合材料构件制孔加工质量,以C/E复合材料为研究对象,提出"以磨代钻"制孔新工艺,并研制了电镀金刚石刀具。与传统硬质合金刀具钻孔工艺进行对比试验,结果表明:金刚石刀具钻削轴向力降低30%-50%、刀具耐用度提高3-5倍、缺陷显著减少,更适合C/E复合材料钻孔加工。Carbon fiber reinforced plastics is one of typical difficult-to-machine materials which will easily bring on disfigurements such as burrs,delamination and avulsion during drilling.In order to improve the drilling quality,the carbon fiber/epoxy(C/E) composite was studied,and a grinding drill and its new process were developed.Some experiments on the grinding tool were carried out.The results show that the thrust force decreases by 30%-50%,the tool life is improved by 3 to 5 times and the disfigurements are minimized compared with the traditional carbide twist drill.

关 键 词:C/E复合材料 “以磨代钻”刀具 钻孔 缺陷 轴向力 

分 类 号:V261.97[航空宇航科学与技术—航空宇航制造工程]

 

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