飞机杆力传感器检测仪研制  

Research and Development of Aircraft Stick Force Sensor Testers

作　　者：严共鸣[1] 王洲伟[1] 赵德春[1] 

机构地区：[1]空军第一航空学院航空机械工程系,河南信阳464000

出　　处：《机械与电子》2016年第5期55-57,共3页Machinery & Electronics

摘　　要：针对某型飞机杆力传感器测试的实际需要,提出了相应的杆力传感器检测仪的设计方案,分析了其基本测试原理和过程,加工制造了该型检测仪并进行了实际测试。结果表明,该型飞机杆力传感器检测仪操作简单,功能完善,智能化程度高,检测快速准确,为飞机杆力传感器性能检测提供了科学的手段,具有较好的推广前景。In response to the practical need for testing control stick force sensors of a certain type of aircraft,the research involves proposing an appropriate design scheme for control stick force sensor testers,analyzing its basic testing principle and process,fabricating the tester,and conducting apractical test.The result shows that the control stick force sensor tester is characterized by easy manipulation,perfect function,and high intelligence,fast and accurate detection,thus providing a scientific testing means for the detecting the performance of the aircraft control stick force sensor and showing good popularizing prospects.

关 键 词：飞机 杆力 传感器 原位检测 

分 类 号：TP212[自动化与计算机技术—检测技术与自动化装置]