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  • 陈果 ( 教授 )

    的个人主页 http://faculty.nuaa.edu.cn/cg1/zh_CN/index.htm

  •   教授   博士生导师
  • 招生学科专业:
    交通运输工程 -- 【招收博士、硕士研究生】 -- 民航学院
    电子信息 -- 【招收博士、硕士研究生】 -- 民航学院
    交通运输 -- 【招收博士、硕士研究生】 -- 民航学院
    交通运输工程 -- 【招收硕士研究生】 -- 通用航空与飞行学院
    交通运输 -- 【招收硕士研究生】 -- 通用航空与飞行学院
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A test method of rotor space bending axis and its test verification

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所属单位:民航学院
发表刊物:Hangkong Dongli Xuebao
摘要:A test method of rotor space bending axis was put forward. Firstly, for a practical bended rotor, the bending of each section centroid relative to the rotation center can be obtained by using the eddy current displacement sensors, and the bending degree of different sections of the rotor can be obtained in the same absolute coordinate system. Secondly, the cubic spline function was applied to fit the space geometry center line of rotor, and the three-dimensional solid models of the bended rotor were shown by using the OPENGL graphics function, which was called by the Visual C++. Finally, the traditional means of measurement based on the dial indicator were employed to verify the proposed method. The results indicated that, the shaft orbit of each section except for section 1 and section 6 measured by the proposed method were consistent with the shaft orbit of the dial indicator, and circle fitting results were also basically coincident. What's more, the error range of the circle fitting of section 1 and section 6 were in reasonable agreement. Thus the method is available to investigate the migration. © 2017, Editorial Department of Journal of Aerospace Power. All right reserved.
ISSN号:1000-8055
是否译文:否
发表时间:2017-09-01
合写作者:Song, Peipei,Dong, Chao,Qu, Meijiao
通讯作者:陈果

 

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