首页 | 本学科首页   官方微博 | 高级检索  
     检索      

用于直升机现场计量的低频振动校准技术
引用本文:杨霖,郑术力.用于直升机现场计量的低频振动校准技术[J].宇航计测技术,2017,37(1):48-54.
作者姓名:杨霖  郑术力
作者单位:1、工业和信息化部电子第五研究所,广州 510610
摘    要:本文面向直升机健康与使用监测系统(HUMS)的现场计量保障需求,针对其中振动传感器在低频段尚无法实现现场校准的现状,提出了基于直线电机驱动技术的便携式低频振动校准技术方案。该方案利用高精度直线电机构造低频标准振动源,采用稳定性高的石英挠性加速度计作为标准加速度计,具有体积小、精度高、现场环境适应性好的特点,非常适用直升机HUMS的现场计量保障。根据不确定度评估结果,该方案能够实现0.5Hz~20Hz频率范围,0.01m/s~2~20m/s~2加速度范围内不超过1%的校准不确定度(k=2)。

关 键 词:健康与使用监测系统    加速度计    低频振动    现场校准    直线电机

On-site Calibration Technique for Helicopter Vibration Sensors in Low Frequency Range
YANG Lin,ZHENG Shu-li.On-site Calibration Technique for Helicopter Vibration Sensors in Low Frequency Range[J].Journal of Astronautic Metrology and Measurement,2017,37(1):48-54.
Authors:YANG Lin  ZHENG Shu-li
Institution:1、China Electronic Product Reliability and Environmental Testing Research Institute,Guangzhou 510610,China
Abstract:This paper presents a technique to fill the void in on-site calibration of accelerometers in helicopter health and usage monitoring systems (HUMS) within low frequency range.The technique employs a compact linear-motor-driven reference vibration exciter and a thermo-stabilized quartz flexible accelerometer to construct a portable,precise,and stable calibrating apparatus,which is quite fit for the on-site calibration of helicopter HUMS. According to the uncertainty estimation and calculation,an expanded calibrating uncertainty (k=2) of no more than 1% is expected of the apparatus over the frequency range of 0.5 Hz~20Hz and the acceleration range of 0.01 m/s2~20 m/s2.
Keywords:Health and usage monitoring systems                                                                                                                        Accelerometers                                                                                                                        Vibration in low frequency range                                                                                                                        On-site calibration                                                                                                                        Linear motor
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航计测技术》浏览原始摘要信息
点击此处可从《宇航计测技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号