| 航空发动机叶片激光冲击处理过程控制研究 |
| |
| 引用本文： | 曹子文,邹世坤,车志刚,许海鹰.航空发动机叶片激光冲击处理过程控制研究[J].航空发动机,2011,37(1):60-62,59. |
| |
| 作者姓名： | 曹子文 邹世坤 车志刚 许海鹰 |
| |
| 作者单位： | 中航工业北京航空制造工程研究所,北京,100024 |
| |
| 摘 要： | 分析了在水约束模式下,光路、约束层、吸收层、靶材等主要因素对激光冲击处理过程控制工艺稳定性的影响。通过研究LSP、MIC、GE、RR等公司在航空发动机叶片激光冲击处理稳定性方面的经验,特别是涉及工艺稳定性的约束控制、光路清理、质量控制等技术,结合叶片激光冲击处理的工艺试验,系统地研究了航空发动机叶片激光冲击处理工艺稳定性的关键控制技术。
|
| 关 键 词： | 激光冲击处理 激光喷丸 航空发动机 叶片 过程控制 |
Research on Process Control of Laser Shock Peening for Aeroengine Blade |
| |
| Authors: | CAO Zi-wen ZOU Shi-kun CHE Zhi-gang XU Hai-ying |
| |
| Institution: | (AVIC Beijing Aeronautical Manufacturing Technology Research Institute,Beijing 100024) |
| |
| Abstract: | The effects of laser path, confining layer, absorbing layer and target on process stability in water-confined laser shock peening were analyzed. In LSP, MIC, GE and RR corporations the experience on aeroengine blade laser shock peening stability,especially the effects of overlay control laser path cleaning and quality eontrol on process stability were investigated. The key control technology of the aeroengine blades in laser shock peening process .stability was systematically summarized by combing with experiments. |
| |
| Keywords: | laser shock peening laser peening aeroengine blade process control |
| 本文献已被 维普 万方数据 等数据库收录！ |
|
