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Publishing Language: Chinese

Research progress on uncertainty effect of compressor blade machining deviation

Limin GAO1( )Haohao WANG1Weina HUANG2Qiusheng LUO2Ruiyu LI1Guang YANG1Yue DAN1Chi MA1Baohai WU3Jiaqi LUO4
School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China
AECC Sichuan Gas Turbine Establishment, Chengdu 610500, China
School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072, China
School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310058, China
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Abstract

The complex three-dimensional configuration and thin-walled structure of compressor blades lead to great difficulty in their manufacturing, and uncertainty of blade geometric deviation is very prominent in the machining process. As the aerodynamic loading of the compressor continues to rise and the geometric size continues to decrease, its working environment and internal flow characteristics become worse and more complex. The harsh working environment amplifies the influence of machining uncertainty. This leads to the high dispersion of the aerodynamic performance for the same batch of compressors and the frequent occurrence of severe performance degradation in service, resulting in substandard performance and even failure problems. In recent years, a lot of research work has been carried out on uncertainty quantification of compressor blade machining deviation at home and abroad. In this paper, the research progress in this field is reviewed in terms of geometric modeling, probabilistic model characterization, uncertainty quantification method, and uncertainty effect. Finally, the key problems and research prospects of uncertainty quantification on compressor blade machining deviation are summarized.

CLC number: V231.3 Document code: A Article ID: 1000-6893(2024)19-630386-22

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Acta Aeronautica et Astronautica Sinica
Article number: 630386

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Cite this article:
GAO L, WANG H, HUANG W, et al. Research progress on uncertainty effect of compressor blade machining deviation. Acta Aeronautica et Astronautica Sinica, 2024, 45(19): 630386. https://doi.org/10.7527/S1000-6893.2024.30386

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Received: 14 March 2024
Revised: 16 April 2024
Accepted: 26 April 2024
Published: 15 October 2024
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica