为研究加工工艺对7075-T7351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,对紧固孔的装配性能和疲劳寿命都有很大的影响.
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