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Publishing Language: Chinese

A contact angle measurement method for torsional teeth

Xiaoyan TONG1( )Dongsheng LU2Hui BAI3Long CHANG4
School of Astronautics,Beihang University,Beijing 100191,China
Aircraft Design and Research Institute,Aviation Industry Harbin Aircraft Industry Group Co.,Ltd.,Harbin 150060,China
Aecc South Industry Company Limited,Zhuzhou 412002,China
Shanghai Aerospace System Engineering Institute,Shanghai 201108,China
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Abstract

The angle measurement of torsional teeth is commonly used in the manufacture and performance test of a helicopter power system. The impact of their coupling on the measurement of torsional teeth angle is examined, as is the influence of installation error caused by the non-alignment between the contact measuring probe and the direct drive motor during the measurement of torsional teeth angle, the error caused by the non-concentricity between the measuring probe and the motor during the installation of torsional teeth, and a contact measuring scheme for measuring torsional teeth angle using a magnetic encoder. A method of angle measurement using redundant observations is proposed and verified by practical angle measurement, which eliminates the influence of the installation errors of torsional teeth and probe on the measurement results, and deduces the angle calculation formula. The results show that the proposed method not only reduces the installation and debugging requirements of the measuring system but also improves the accuracy of angle measurement for the torsional teeth, making it suitable for similar precise angle measurements.

CLC number: TB22 Document code: A Article ID: 1001-5965(2026)01-0104-06

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Journal of Beijing University of Aeronautics and Astronautics
Pages 104-109

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Cite this article:
TONG X, LU D, BAI H, et al. A contact angle measurement method for torsional teeth. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(1): 104-109. https://doi.org/10.13700/j.bh.1001-5965.2023.0721

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Received: 03 November 2023
Published: 20 November 2023
© Journal of Beijing University of Aeronautics and Astronautics