宇航计测技术 ›› 2019, Vol. 39 ›› Issue (2): 1-5.doi: 10.12060/j.issn.1000-7202.2019.02.01

• 论文 •    下一篇

转动惯量测量研究的进展及展望

王小三1；刘云平1；倪怀生1；张宁2   

  1. 1、北京航天计量测试技术研究所，北京 100076；
    2、上海商用航空发动机有限责任公司，上海 200000
  • 出版日期:2019-04-25 发布日期:2019-04-25
  • 作者简介:王小三（1976-），男，硕士，研究员，主要研究方向：力学计量技术。

Progress and Prospects for the Measurement Research on the Moment of Inertia

WANG Xiao-san1；LIU Yun-ping1；NI Huai-sheng1；ZHANG Ning2   

  1. 1、Beijing Aerospace Institute for Metrology and Measurement Technology, Beijing 100076，China；
    2、AECC Commercial Aircraft Engine CO.LTD,Shanghai 200000,China
  • Online:2019-04-25 Published:2019-04-25

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摘要： 对转动惯量测量的研究情况作了综述，对三线摆法、扭摆法、落体法等转动惯量测量方法的测量原理及其优缺点进行了总结，介绍了针对以上缺点的一种新的测量方法，预测该方法将代表转动惯量测量的发展方向。

关键词: 转动惯量, 研究进展, 扭摆法, 空气阻尼

Abstract: A review on the measurement research of the moment of inertia is carried out. The principles of some current measurement methods of the moment of inertia, such as the trilinear pendulum method, the torsion pendulum method and the falling body method, are summarized as well as their advantages and disadvantages. A new method aimed at these disadvantages is introduced, which is prospected to be a development direction for the measurement of the moment of inertia.

Key words: Moment of inertia, Research progress, Torsion pendulum method, Air damping

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