• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2023, Vol. 59 ›› Issue (17): 349-360.doi: 10.3901/JME.2023.17.349

• 制造工艺与装备 • 上一篇    

扫码分享

航发叶片砂碟磨削接触特性及材料去除机理

段继豪1, 安佳乐1, 吴卓繁1, 淮文博2, 高峰1   

  1. 1. 西安理工大学陕西省机械制造装备重点实验室 西安 710048;
    2. 西安理工大学工程训练国家级实验教学示范中心 西安 710048
  • 收稿日期:2023-01-11 修回日期:2023-05-08 出版日期:2023-09-05 发布日期:2023-11-16
  • 通讯作者: 段继豪(通信作者),男,1985年出生,博士,讲师。主要研究方向为数控精密磨削加工。E-mail:djh@xaut.edu.cn
  • 作者简介:安佳乐,男,1997年出生,硕士研究生。主要研究方向为精密磨削加工控制。E-mail:568662044@qq.com;吴卓繁,男,2000年出生,硕士研究生。主要研究方向为磨削加工。E-mail:1273120496@qq.com;淮文博,男,1979年出生,博士,副教授。主要研究方向为先进数控加工技术。E-mail:huaiwb@xaut.edu.cn;高峰,男,1969年出生,博士,教授,博士研究生导师。主要研究方向为数控机床设计与制造。E-mail:gf2713@xaut.edu.cn
  • 基金资助:
    陕西省重点研发计划(2021ZDLGY09-01)、陕西省自然科学基础研究计划(2023-JC-YB-434、2022JM-240)和陕西省教育厅自然科学专项(19JK0593)资助项目。

Contact Characteristics and Material Removal Mechanism of Abrasive Disc Grinding of Aero-engine Blade

DUAN Jihao1, AN Jiale1, WU Zhuofan1, HUAI Wenbo2, GAO Feng1   

  1. 1. Key Lab of Manufacturing Equipment of Shaanxi Province, Xi'an University of Technology, Xi'an 710048;
    2. National Experimental Demonstration Teaching Center for Engineering Training, Xi'an University of Technology, Xi'an 710048
  • Received:2023-01-11 Revised:2023-05-08 Online:2023-09-05 Published:2023-11-16

摘要: 航空发动机叶片型面曲率复杂变化、薄壁结构加工刚性弱,使其精密磨削接触状态多变、磨具轨迹规划困难,引起加工表面质量一致性差。为实现叶片磨削工艺优化,基于叶片磨削工艺特点分析,开展叶片砂碟磨削工艺接触特性及材料去除机理研究,利用降维法建立砂碟磨削材料去除率理论模型,通过砂碟磨削接触特性以及材料去除过程仿真研究,揭示了砂碟磨削不同工艺参数对叶片法向接触压力分布、等效法向接触压力、接触面积、接触轮变形及材料去除深度的影响规律,结合砂碟磨削工艺试验,对仿真结果进行验证。研究结果表明,砂碟磨削接触倾角与法向接触压力、接触面积呈负相关,与接触轮最大变形量呈正相关,接触倾角从10°增大到30°,本质使磨具更加锋利,材料去除深度峰值增大约59.78%,有效磨削区域显著降低;随着磨削深度从0.1 mm增大至0.3 mm,法向接触压力、接触面积及接触轮最大变形量均增大,有效磨削区域显著增大,材料去除深度峰值增大1.57倍,达到0.188 mm;接触倾角与磨削深度是影响砂碟磨削材料去除的主要因素,对获得高质量表面并实现磨削工艺控制具有重要的作用。

关键词: 航发叶片, 砂碟磨削, 接触特性, 材料去除率

Abstract: The complex curvature of blade profile and weak machining rigidity of thin-wall structure make it difficult to plan trajectory of grinding tools under the condition of variable contact state, resulting in poor machining consistency accordingly. In order to realize the optimization of blade grinding process, the contact characteristics and material removal mechanism of blade abrasive disc grinding process are studied on the basis of blade grinding characteristics. Firstly, the theoretical model of material removal rate is established based on method of dimensionality reduction. The influence of different process parameters on normal contact pressure distribution, equivalent contact force, contact area, deformation of contact wheel and material removal depth are revealed by means of simulation and experiments. The research results show that there is a negative correlation between inclination angle and normal pressure or contact area, and a positive correlation between inclination angle and maximum deformation of contact wheel. Increasing the inclination angle from 10° to 30° essentially makes abrasive tool sharper. Consequently, the maximum material removal depth increases by about 59.78%, and the effective grinding area is significantly reduced. With the increase of grinding depth from 0.1 mm to 0.3 mm, the normal contact pressure, contact area, contact wheel deformation and effective grinding area increase significantly. And the maximum material removal depth increases by 1.57 times to 0.188 mm. Inclination angle and grinding depth are the main factors affecting material removal rate in abrasive disc grinding, which play an important role in obtaining high quality surface and realizing real-time control of grinding process.

Key words: aero-engine blade, abrasive disc grinding, contact characteristics, material removal rate

中图分类号: