基于滚压强化的钛合金零件工艺改进

朱朝晖 刘进明

金属功能材料 ›› 2015, Vol. 22 ›› Issue (5) : 57-59.

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金属功能材料 ›› 2015, Vol. 22 ›› Issue (5) : 57-59. DOI: 10.13228/j.boyuan.issn1005-8192.2015063

基于滚压强化的钛合金零件工艺改进

  • 朱朝晖, 刘进明
作者信息 +

Process improvement of titanium alloy parts based on rolling strengthening

  • ZHU Zhao- hui,LIU Jin- ming
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文章历史 +

摘要

为了提高Ti- 6Al- 4V零件的疲劳强度,采用滚压强化的工艺方法加工零件的过渡圆角和螺纹。针对零件滚压后出现了表面缺口及表面裂纹等缺陷,从零件的技术要求入手分析不合格原因,改进了工艺,使得产品合格率从86.7%上升到了96%,并对该工艺改进进行了讨论,提供了可借鉴的经验。

Abstract

In order to improve the fatigue strength of Ti- 6Al- 4V parts,the transition fillet and the thread of the parts are worked by rolling strengthening process. However, notch and crack defects appeared on surface after rolling. So the reason for the failure of the transition fillet and the thread surface is analyzed from the technical requirements analysis, the product qualification rate is greatly raised from 86.7% to 96% after the process improvement. Three referential experiences are provided after the process improvement was discussed.

关键词

关键词:疲劳强度 / 滚压强化 / 裂纹 / 粗糙度

Key words

Keywords: fatigue strength / rolling strengthening / crack / surface roughness

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导出引用
朱朝晖, 刘进明. 基于滚压强化的钛合金零件工艺改进[J]. 金属功能材料, 2015, 22(5): 57-59 https://doi.org/10.13228/j.boyuan.issn1005-8192.2015063
ZHU Chao-Hui, LIU Jin-Ming. Process improvement of titanium alloy parts based on rolling strengthening[J]. Metallic Functional Materials, 2015, 22(5): 57-59 https://doi.org/10.13228/j.boyuan.issn1005-8192.2015063

参考文献

[1] R.R. Boyer. An overview on the use of titanium in the aerospace industry, Journal of Materials Science and Engineering, A213 (1996) 103-114.
[2] V. Venkateswarlu, D. Tripathy, K. Rajagopal et al. Failure analysis and optimization of thermo-mechanical process parameters of titanium alloy(Ti-6Al-4V)fasteners for aerospace applications, Journal of Case Studies in Engineering Failure Analysis, 1 (2013) 49–60
[3] 黄新跃,胡本润,吴学仁等.钛合金Ti-6Al-4V两种微观结构的裂纹扩展行为研究[J].机械强度, 2002, 24(4):584- 587.
[4] 王晓森,高行山,孙贤等.冷挤压对钛合金紧固结构件的耐久性影响研究[J].机械科学与技术, 2012,31(10):1601-1604
[5] 段学政,高扬,张振民等.TC4钛合金风扇盘裂纹分析[J].航空材料, 1986, 3: 30-33.
[6] 陶春虎, 刘庆瑔等. 航空用钛合金的实效及其预防[M].北京: 国防工业出版社, 2002, 114-139,186-192
[7] GB/T 5779.3-2000. 紧固件表面缺陷 螺栓、螺钉和螺柱 特殊要求[S]
[8] 傅旭强. 加氢压缩机二级活塞杆断裂失效分析[J].化工设备与管道, 2006,43(3): 52-54.
[9] 陈永富, 杨成贞.钛合金对接螺栓螺纹滚压加工[J].机械工艺师, 1998,11: 14-15
[10] 张秀梅. 浅谈螺纹滚压加工技术[J].中国新技术新产品, 2012,12:149.
[11] 章锦如. TC4钛合金中的偏析[J].稀有金属, 1980,1:17-21
[12] 常璐, 夏金华, 陈绍凯.钛合金材料夹杂和偏析缺陷的实验表征[J]. 西安文理学院学报, 2011,14(1):57-58
[13] YX Cui, QC Meng, BY Zhang et al. Fracture analysis of Ti-6Al-4V bolts, Journal of Engineering Failure Analysis, 13 (2006) 669–672

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