摘要
为研究加工工艺对 70 75 T73 5 1铝合金飞机装配紧固孔表面质量的影响 ,通过扫描电子显微镜和光学显微镜 ,分别对 5种不同制孔工艺所产生的表面微观形貌和表层组织变化进行了观察和分析。结果表明 ,钻扩铰多步慢进给工艺和一步复合制孔工艺所加工出的表面 ,平整、光滑、加工缺陷少、晶格变形小、变质层薄 ;而其它工艺条件下 ,孔表面微观形貌复杂、加工纹路紊乱、表面缺陷多、晶格畸变大 ,变质层厚 ,这些加工状况 。
In order to study the effect of machining processes on the surface condition of fastening holes drilled on 7075 aluminum alloy for aircraft assembly, the surface microphotograph and surface layers microstructure produced by the five kinds of drilling processes were observed and analyzed by means of SEM and optical microscope. The results show that the surface microphotograph yielded in multiple step machining with slow feeding and in one step compound process is satisfactory, and there are fewer defects, lower deformation and thinner metamorphic layers; while that produced in other processes is quite rough, there are more defects and bigger deformation on the machined surface, and they are detrimental to assembly properties and fatigue life of fastening holes.
出处
《中国有色金属学报》
EI
CAS
CSCD
北大核心
2001年第4期655-660,共6页
The Chinese Journal of Nonferrous Metals
关键词
铝合金
紧固孔
加工工艺
微观形貌
显微组织
加工缺陷
飞机
aluminum alloy
fastening hole
machining processes
microphotograph
microstructure
machining defect
