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旋翼天平原位校准的不确定度分析
引用本文:汤斌,肖彬,张文静,王建强.旋翼天平原位校准的不确定度分析[J].计测技术,2021,41(2):194-199.
作者姓名:汤斌  肖彬  张文静  王建强
作者单位:航空工业北京长城计量测试技术研究所, 北京100095;航空工业直升机设计研究所, 江西 景德镇333001
摘    要:旋翼天平原位校准中,校准不确定度是最核心的技术指标.根据实际工况环境,研究了原位校准方法,研制了原位校准装置,重点介绍了机械设计结构,梳理和明确了不确定度来源,最后完成了旋翼天平的首次原位校准测试工作,并依照规范的方法进行了原位校准不确定度评价,结果表明:校准装置性能达标,各力值分量相对校准不确定度均优于0.1%,各力...

关 键 词:旋翼天平  多分量气动力  原位校准  不确定度  加载头

Uncertainty Analysis of Rotor Balance In-situ Calibration
Abstract:In the in-situ calibration of rotor balance, the calibration uncertainty is the most important technical factor. First, the environment according to the actual working condition and in-situ calibration method is studied. Then, the in-situ calibration device was developed, mainly introducing the mechanical structure design and ascertaining the sources of uncertainty. Finally, for the first time in-situ calibration test of the rotor balance was completed and for in-situ calibration uncertainty was evaluated in accordance with the standard method. The results showed that the standard calibration device has achieved that the relative force-component calibrating uncertainty is better than 0.1%, the relative torque component calibrating uncertainty is better than 0.3%.
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