Research on Abrasive Flow Polishing Technology and Quality Control of High Performance Impeller Surface

Author:

Li Junye1,Tang Jiaxu1,Liu Jianhe1,Qu Jiyong1,Zhang Xinming2,Xu Chengyu1

Affiliation:

1. Changchun University of Science and Technology

2. Foshan University

Abstract

Abstract The rapid development of science and technology puts forward higher requirements for the quality and accuracy of high-performance impeller parts. In order to improve the machining accuracy of the inner surface and enhance the uniformity of the whole structure, In this paper, the large eddy simulation method is used to simulate and analyze the abrasive flow machining process of the high performance impeller with different machining parameters. Then the three processing parameters of inlet pressure, inlet speed and abrasive viscosity are simulated numerically. The results show that increasing the inlet pressure and abrasive viscosity can effectively improve the processing effect. Increasing the inlet speed will improve the processing intensity, but the overall processing uniformity will be reduced. The experiment result shows: The inlet pressure and particle size have a significant impact on the abrasive flow machining effect, followed by the number of machining times, and the surface roughness of the high-performance impeller after abrasive flow machining can reach 0.052µm, and the best technological parameters determined by the experimental research can realize the uniform polishing of the high performance impeller by abrasive flow machining technology.

Publisher

Research Square Platform LLC

Reference24 articles.

1. Li W, Wen X, Li X, Yang S. Application and development trend of remanufacturing technology for aero-engine blades[J]. Diamond & Abrasives Engineering, 2021,41(04):8–18. https://doi.org/10.13394/j.cnki.jgszz.2021.4.0002

2. Qi Y, Feng X, Su B, et al. Analysis and control of machining deformation of aero-engine blades[C]. Proceedings of the 17th Shenyang Scientific Annual Conference,2020:698–700. https://doi.org/10.26914/c.cnkihy.2020.012047

3. Aero-engine blade and its development trend[J];Sun F;Shandong Industrial Technology,2018

4. Analysis and control of deformation factors in aero-engine blade machining[J];Huang C;Plant Maintenance Engineering,2020

5. Characteristics and application of abrasive flow machining technology[J].Metal Working(Cold working),2009;Zhan H

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3