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涡轮叶尖激光熔覆涂层技术探索

Research of laser cladding coating on turbine blade tip

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【作者】 孟庆武杨胜群耿林曲伸祝文卉刘佳涛

【Author】 MENG Qing-wu1,YANG Sheng-qun2,GENG Lin1,QU Shen2,ZHU Wen-hui2,LIU Jia-tao2(1.Harbin Institute of Technology,Harbin 150001,China;2.Shenyang Liming Aero-Engine Corporation,Shenyang 110043,China)

【机构】 哈尔滨工业大学沈阳黎明航空发动机公司

【摘要】 为了探索涡轮叶尖端部型腔涂层的制备工艺,以堆焊用镍基合金焊条加工成的粉末为原材料,分别采用激光熔覆及氩弧堆焊技术,在铸造镍基合金试样表面上制备涂层.结果表明:激光熔覆涂层在成型性上优于堆焊涂层,激光熔覆涂层的组织细小致密,硬度高于堆焊涂层的硬度;在涡轮叶尖上进行激光熔覆涂层工艺探索也获得成功.

【Abstract】 In order to research a model structure coating on turbine blade tip,a laser cladding coating and an argon-arc surfacing welding coating were deposited on surface of casting Ni-base alloy samples.A kind of powder made of Ni-base alloy surfacing welding rod was used in laser cladding technology.The experimental results indicate that the material forming of the laser cladding coating is better than that of the argon-arc surfacing welding coating.The microstructure of laser cladding coating is fine and dense.The hardness of laser cladding coating is higher than that of surfacing welding coating.By means of laser cladding technology,a model structure coating was deposited on turbine blade tip.

【关键词】 涡轮叶尖激光熔覆镍基合金涂层
【Key words】 turbine blade tiplaser claddingNi-base alloycoating
【基金】 黑龙江省博士后专项基金资助(LBH-Z07167)
  • 【文献出处】 材料研究与应用 ,Materials Research and Application , 编辑部邮箱 ,2009年02期
  • 【分类号】TG44
  • 【被引频次】10
  • 【下载频次】285
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