整体叶盘损伤叶片修复加工的几何模型重构与加工误差控制技术研究进展

党稼宁; 范凌松; 李飞; 张永刚; 张莹; 吴宝海

doi:10.16080/j.issn1671-833x.25010186

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整体叶盘损伤叶片修复加工的几何模型重构与加工误差控制技术研究进展

论坛 | 更新时间：2026-06-16

- 整体叶盘损伤叶片修复加工的几何模型重构与加工误差控制技术研究进展
- 航空制造技术 2026年69卷第10期页码：54-74
- 作者机构：
  
  西北工业大学航空发动机高性能制造工信部重点实验室，西安 710072
  西北工业大学航空发动机先进制造技术教育部工程研究中心，西安 710072
  西北工业大学硬质合金全国重点实验室，西安 710072
  中国航发动力股份有限公司，西安 710021
  西安西航集团莱特航空制造技术有限公司，西安 710018
- 作者简介：
  
  吴宝海，教授，博士生导师，研究方向为高性能制造及智能加工技术。
- 基金信息：
- DOI：10.16080/j.issn1671-833x.25010186
  中图分类号： V232
- 收稿：2025-12-15，
  
  修回：2026-01-12，
  
  录用：2026-02-02，
  
  纸质出版：2026-05-15
- 稿件说明：
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引文格式：党稼宁，范凌松，李飞，等.整体叶盘损伤叶片修复加工的几何模型重构与加工误差控制技术研究进展[J].航空制造技术，2026, 69（10）：25010186.

DANG Jianing, FAN Lingsong, LI Fei, et al. Geometric model reconstruction and machining error control for repair technologies of damaged blisk blades: Recent advances and future trends[J]. Aeronautical Manufacturing Technology, 2026, 69(10): 25010186.
引文格式：党稼宁，范凌松，李飞，等.整体叶盘损伤叶片修复加工的几何模型重构与加工误差控制技术研究进展[J].航空制造技术，2026, 69（10）：25010186. DOI： 10.16080/j.issn1671-833x.25010186.

DANG Jianing, FAN Lingsong, LI Fei, et al. Geometric model reconstruction and machining error control for repair technologies of damaged blisk blades: Recent advances and future trends[J]. Aeronautical Manufacturing Technology, 2026, 69(10): 25010186. DOI： 10.16080/j.issn1671-833x.25010186.

摘要

整体叶盘作为新一代航空发动机的核心部件，其一体化轻量结构在提升推重比和气动效率方面优势显著。然而，在极端服役环境下，叶片易遭受外物打击、高温氧化、高周疲劳等多种损伤。由于一体化结构特性，受损叶片无法单独更换，使得维护成本高昂，严重制约了整体叶盘的批产应用。叶片修复加工技术可高效、低成本地恢复损伤叶片性能、延长服役寿命，已成为推动整体叶盘大规模应用的关键使能技术。本文综述了整体叶盘损伤叶片修复加工技术的研究现状与发展方向，在介绍叶片损伤类型与修复工艺流程的基础上，分析了损伤叶片几何模型重构与气动性能提升的理论方法，进而围绕损伤叶片修复加工弹性变形控制问题，归纳了薄壁零件铣削加工弹性变形预测和弹性变形补偿的研究进展及存在问题，最后展望了损伤叶片修复加工未来发展趋势。

Abstract

As a critical component of next-generation aero-engines

the blisk offers substantial advantages in thrustto-weight ratio and aerodynamic efficiency owing to its monolithic lightweight architecture. However

under extreme operating conditions

blisk blades are highly susceptible to various forms of damage

including foreign object damage

hightemperature oxidation

and high-cycle fatigue. The inherent monolithic nature of the blisk precludes the replacement of individual damaged blades

resulting in prohibitively high maintenance costs that severely impede its large-scale production and deployment. Blade repair and remanufacturing technology provides an efficient and cost-effective pathway to restore the performance of damaged blades and extend their service life

and has thus emerged as a key enabling technology for the widespread engineering application of blisks. This paper presents a review of the current research status and future development directions of blisk blade repair technology. Building upon an introduction to blade damage typology and repair process workflows

the theoretical methodologies for geometric model reconstruction and aerodynamic performance recovery of damaged blades are systematically analyzed. Subsequently

with a focus on elastic deformation control during blade repair machining

the research advances and existing challenges in elastic deformation prediction and compensation for thin-walled component milling are thoroughly examined. Finally

prospective development trends in damaged blade repair and remanufacturing technology are discussed.

关键词

Keywords

references

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