Geometric Error Analysis of Compressor Blade Based on Reconstructing Leading and Trailing Edges Smoothly

Yaohua Hou, Ying Zhang, Dinghua Zhang

科研成果: 期刊稿件会议文章同行评审

7 引用 (Scopus)

摘要

In the process of blade design, the shape of blade, which causes great influence on aerodynamic performance, is the most difficult part for designer. The shape of blade changes because of the cutting force, residual stress and deformation. To analyze the precise error of this, this paper presents a new algorithm for reconstructing cross section curve of blade from measuring points. The Gauss-Newton method and dichotomy are used to fit the circle of leading and trailing edge, which is the most important part of blade. Then the deformation error, contour error and parameter error are calculated with relative algorithm based on the new cross section curve. Also, a series of points and a blade model are utilized to demonstrate the effectiveness of this novel algorithm on reconstructing cross section curve and analyzing machining error.

源语言英语
页(从-至)272-278
页数7
期刊Procedia CIRP
56
DOI
出版状态已出版 - 2016
活动9th International Conference on Digital Enterprise Technology - Intelligent Manufacturing in the Knowledge Economy Era, DET 2016 - Nanjing, 中国
期限: 29 3月 201631 3月 2016

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