扩压器套料电解加工绝缘套结构刚度优化研究
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作者单位:

南京航空航天大学机电学院,南京 210016

作者简介:

通讯作者:

朱栋,男,教授,博士生导师,E-mail:zhudong@nuaa.edu.cn。

中图分类号:

TG662

基金项目:

国家自然科学基金重大研究计划培育项目(91860135);国家科技重大专项(2017-Ⅶ-0004-0097)。


Study on Structural Stiffness Optimization of Insulating Sleeve for Electrochemical Trepanning of Diffuser
Author:
Affiliation:

College of Mechanical and Electronic Engineering, Nanjing University of Aeronautics & Astronautics, Nanjing 210016,China

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    摘要:

    扩压器是航空发动机压气机的关键部件,对发动机性能、效率及运行工况有重要影响。为解决扩压器套料电解加工过程中绝缘套结构刚性差易变形进而影响加工稳定性的问题,提出了绝缘套刚性优化方法,在绝缘套自由端处设计了加强筋结构,开展了不同加强筋形状、尺寸下的流固耦合仿真对比研究。当加强筋两端为圆形、宽度b=2 mm、距底端距离h=6 mm时,与未设置加强筋结构相比,最大变形量减少了88.3%。研制了带加强筋的扩压器套料电解加工绝缘套及阴极结构,开展电解加工试验研究,实现了阴极进给速度为1.4 mm/min稳定加工,加工稳定性和效率显著改善,验证了绝缘套刚性优化方法的有效性。

    Abstract:

    Diffuser is a key component of aero-engine compressor, which has an important impact on its performance, efficiency and operating conditions. In order to solve the problem of poor rigidity and easy deformation of insulating sleeve structure in the process of electrochemical trepanning, the optimization method of insulating sleeve rigidity is proposed, strengthening rib is designed at the free end of insulating sleeve, and the fluid structure coupling simulation comparative study under different strengthening rib shapes and sizes is carried out. When the two ends of strengthening rib are round, the width b = 2 mm and the distance from the bottom h = 6 mm, the maximum deformation is reduced by 88.3% compared with the structure without strengthening rib. The experimental research of electrolytic machining is carried out. The stable machining with cathode feed rate of 1.4 mm/min is realized, and the machining stability and efficiency are significantly improved. The effectiveness of the rigidity optimization method of insulating sleeve is verified.

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引用本文

李正寅,朱栋,张晓博.扩压器套料电解加工绝缘套结构刚度优化研究[J].南京航空航天大学学报,2022,54(3):378-386

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  • 收稿日期:2022-04-10
  • 最后修改日期:2022-05-18
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  • 在线发布日期: 2022-06-05
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