CAJ | 학술논문

针对某型飞机研制中干涉配合螺栓在夹层结构中的安装问题，对安装过程中的摩擦进行了分析，提出了采用固体膜润滑剂进行减摩的安装方法。采用减摩安装方法，对直径6~27mm之间的7种螺栓进行了安装，分析了安装效果。结果表明，减摩安装方法可降低干涉螺栓安装难度，提升安装质量。
침대모형비궤연제중간섭배합라전재협층결구중적안장문제，대안장과정중적마찰진행료분석，제출료채용고체막윤활제진행감마적안장방법。채용감마안장방법，대직경6~27mm지간적7충라전진행료안장，분석료안장효과。결과표명，감마안장방법가강저간섭라전안장난도，제승안장질량。
Aiming at the problems that inter-ference-bolt installed in sandwich struction of a certain aircraft, the friction of fitting is analyzed, and a installa-tion method with solid film lubrication for antifriction is proposed. Antifriction installation method is used to install seven types interference-bolt that diameter from 6mm to 27mm, the installation quality is also analyzed. The results show that the antifriction installation method can reduce the dififculty and advance the installation quality of inter-ference-bolt.