摘要
估算了高加速寿命试验应力对一种飞机刹车控制装置的作用时间，并和首翻期内使用应力的作用时间进行比较，实现了将高加速寿命试验数据用于寿命与可靠性评估的目的。
The actuation duration of highly accelerated life testing stress on the brake control device of an air- craft is estimated and compared with the time of operating stress during the course of first overhaul. The pur- pose of applying highly accelerated life testing data to evaluate the life and reliability of the aircraft brake con- trol device is realized.
作者
乔建军
乔子骅
焦坤
李晓猛
彭娟
张宏艳
QIAO Jian-jun;QIAO Zi-hua;JIAO Kun;LI Xiao-meng;PENG Juan;ZHANG Hong-yan(AVIC Xi＇an Aviation Brake Technology Co.,Ltd,Xi＇an 710075,China;The 39th Research Institute of China Electronic Technology Group Corporation,Xi＇an 710077,China)
出处
《测控技术》
CSCD
2018年第B11期103-106,共4页
Measurement & Control Technology
关键词
高加速寿命试验
过程测试
累积损伤
可靠性评估
highly accelerated life testing
procedural test
cumulative damage
reliability evaluation
