| 尾轴花键高强度涂层修复工艺研究 |
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| 引用本文： | 张胜宝,师玉英,张旭,朱立群.尾轴花键高强度涂层修复工艺研究[J].表面技术,2011,40(4):69-71,107. |
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| 作者姓名： | 张胜宝 师玉英 张旭 朱立群 |
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| 作者单位： | 中航工业哈尔滨东安集团有限公司,哈尔滨,150066;北京航空航天大学材料科学与工程学院,北京,100083 |
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| 摘 要： | 通过工艺试验,确定了高强度丽绚涂层塑化阶段的工艺路线和工艺参数,使尾轴花键的涂层能够在整体状况下进行修复,并且进行了性能试验以及疲劳试验,解决了飞机飞行故障,消除了丽绚涂层脱落对飞机性能的影响.
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| 关 键 词： | 丽绚 涂层 塑化 疲劳试验 |
The Repair Technical Study of Caudal Roller Spline High Intensity Rilsan Coat |
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| ZHA NG Sheng-bao,SHI Yu-ying,ZHANG Xu,ZHU Li-qun.The Repair Technical Study of Caudal Roller Spline High Intensity Rilsan Coat[J].Surface Technology,2011,40(4):69-71,107. |
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| Authors: | ZHA NG Sheng-bao SHI Yu-ying ZHANG Xu ZHU Li-qun |
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| Affiliation: | 1.AVIC Harbin Dongan Engine(group) Corporation LTD,Harbin 150066,China;2.School of Materials Science and Engineering,Beihang University,Beijing 100083,China) |
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| Abstract: | The technics confirms the technics folw and technics parameter of high intensity Rilsan coat by large numbers of experiment,the research cause of coat of caudal roller can be holistic repair,and carry through large numbers of capability experiment and fatigue test,it raveled out the fault of plane,eliminated the infection plane capability of break off of Rilsan coat. |
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| Keywords: | rilsan coat plasticization fatigue test |
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