飞机全机主操纵系统与机体同时进行疲劳试验的联调测试及试验监控  

Join-Test Verification and Monitoring Analysis Method of the Primary Flight Control System Fatigue Test Together with Whole-Airframe Fatigue Test

作　　者：卢京明 

机构地区：[1]中航第一飞机研究院强度研究所,陕西西安710089

出　　处：《飞机设计》2009年第3期9-13,17,共6页Aircraft Design

摘　　要：针对某型飞机全机主操纵系统疲劳试验与机体疲劳试验在同一架飞机上同时进行的有关问题进行了讨论,并就全机主操纵系统与机体疲劳同试时的联调测试及试验监控分析方法确定进行了阐述。联调测试和系统疲劳试验结果表明:全机主操纵系统与机体两项独立的疲劳试验可以同时进行;系统疲劳试验所用的监控分析方法实用有效。A study of the join - test verification and monitoring analysis method of the primary flight control system fatigue test, together with the whole - airframe fatigue test on the same aircraft, is presented, and the relevant problems of the primary flight control system fatigue test with the whole - airframe fatigue test is discussed. The join - test results show that the two different kinds of fatigue tests can be done respectively at the same time. The method of the monitoring analysis for the primary flight control system fatigue test has been proved to be effective and available.

关 键 词：飞机 主操纵系统 机体 疲劳试验 联调测试 试验监控分析方法 

分 类 号：V216.3[航空宇航科学与技术—航空宇航推进理论与工程]