China Mechanical Engineering ›› 2025, Vol. 36 ›› Issue (12): 3047-3056.DOI: 10.3969/j.issn.1004-132X.2025.12.030

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Technology on Flexible Polishing for Leading and Trailing Edges of Blisk Blades

Chengshuo LIU1(), Xiaojun LIN2, Bo ZHONG1, Wenhui DENG1   

  1. 1.Laser Fusion Research Center,China Academy of Engineering Physics,Mianyang,Sichuan,621900
    2.Key Laboratory of High Performance Manufacturing for Aero Engine,Ministry of Industry and Information Technology,Northwestern Polytechnical University,Xi'an,710072
  • Received:2025-02-12 Online:2025-12-25 Published:2025-12-31
  • Contact: Chengshuo LIU

整体叶盘叶片前后缘柔性抛光技术

刘承硕1(), 蔺小军2, 钟波1, 邓文辉1   

  1. 1.中国工程物理研究院激光聚变研究中心, 绵阳, 621900
    2.西北工业大学航空发动机高性能制造工业和信息化部重点实验室, 西安, 710072
  • 通讯作者: 刘承硕
  • 作者简介:刘承硕*(通信作者),男,1999年生,助理工程师。研究方向为航空发动机复杂薄壁件精密加工、先进光学制造、离子束抛光。E-mail:1755483268@qq.com
  • 基金资助:
    中物院科学技术发展基金(TCGH0812)

Abstract:

Aiming at the problems of low polishing efficiency, difficulty in ensuring surface quality and profile accuracy of the leading and trailing edges of aero-engine blades, a study on the automated polishing processes for the leading and trailing edges of blisk blades was conducted. The influence of processing parameters on the size of the polishing contact area at the leading and trailing edges was analyzed, and a predictive model for normal polishing force was established, with a root mean square error of 1.24 N between the predicted and actual values. Based on the Preston equation, the effects of compression amount, spindle speed, sponge abrasive wheel radius, feed rate, and abrasive grit size on material removal in the polishing contact area were modeled. Experiments were conducted using the proposed predictive model for material removal depth at the leading and trailing edges. The experimental results show that the value of surface roughness of the blade leading and trailing edges is reduced to 0.18 μm, verifying that the predictive model may effectively forecast material removal depth. Additionally, the sponge abrasive wheel is proven to effectively improve the surface roughness of the blade leading and trailing edges.

Key words: leading and trailing edges of blisk blade, polishing contact zone, material removal, roughness

摘要:

针对航空发动机叶片前后缘抛光加工效率低、表面质量及轮廓精度难以保证等问题开展了整体叶盘叶片前后缘自动化抛光工艺研究。分析了工艺参数对前后缘抛光接触区域尺寸的影响规律,建立了法向抛光力预测模型,预测值与实际值均方根误差为1.24 N;基于Preston方程对抛光接触区域内压缩量、主轴转速、海绵砂圈半径、进给速度和磨具粒度对材料去除的影响规律进行了建模。基于所提出的前后缘抛光材料去除深度预测模型进行实验,结果表明,叶片前后缘表面粗糙度降低至0.18 μm,验证了该预测模型可以有效地预测材料去除深度,海绵砂圈可以有效改善叶片前后缘粗糙度。

关键词: 整体叶片前后缘, 抛光接触区域, 材料去除深度, 粗糙度

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