全尺寸飞机机体疲劳试验时中央翼与外翼连接区域疲劳损伤的声发射监测  

AE Monitoring of Damages of Central Wing and Outer Panel Jointing Area During Full-scale Aircraft Body Fatigue Test

作　　者：耿荣生[1] 吴克勤[2] 景鹏[1] 傅刚强[1] 

机构地区：[1]北京航空工程技术研究中心,北京100076 [2]东北大学机械工程与自动化学院,沈阳110004

出　　处：《无损检测》2008年第1期37-41,共5页Nondestructive Testing

摘　　要：中央翼-外翼连接区域是某型飞机全尺寸疲劳试验需特别关注的部位,其中φ10mm垂直方向对接销钉和孔以及φ12mm水平方向对接螺栓和孔等,或因形状特殊无法使用超声波探伤,或者因不可达而无法应用常规无损检测技术检查。介绍了使用声发射技术对该部位的跟踪监测。利用趋势分析、基于时间、空间的滤波和基于幅度和能量分布等多种信号处理方式,以及多参数综合识别技术,对这些关键部位的状态进行了声发射连续跟踪监测,为保证机体部件疲劳试验的顺利进行起到重要作用。The central wing and outer panel jointing area was the key structure to be monitored during the full-scale aircraft fatigue test. The  φ10 mm vertical and  φ12 mm horizontal bolts, and their corresponding holes, were of special concern during the test because of the difficulties faced by conventional non-destructive testing means to inspect them and evaluate their damages. Due to the inaccessibility, complex structures and very high sound wave attenuation of these parts, the work of AE monitoring was conf...

关 键 词：声发射检测 全尺寸飞机 疲劳试验 疲劳损伤 趋势分析 

分 类 号：TG115.28[金属学及工艺—物理冶金]