首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基体预热温度对ZrO2 涂层结合强度的影响
引用本文:王德朋,李庆会,王旭东.基体预热温度对ZrO2 涂层结合强度的影响[J].宇航材料工艺,2010,40(3).
作者姓名:王德朋  李庆会  王旭东
作者单位:第二炮兵青州士官学校工程系,青州,262500
摘    要:用等离子喷涂的方法在不同温度的45#钢基体上制备ZrO2涂层,通过涂层的结合实验、X射线衍射分析了基体温度与涂层结合强度之间的关系,发现当基体预热温度为250℃时涂层的结合强度最高,可达13.4 MPa;当预热温度高于350℃时,粘结层中的热生长氧化物明显增加,导致涂层的结合强度降低。

关 键 词:热障涂层  等离子喷涂  基体预热温度  结合强度

Eeffect of Substrate Preheating Temperature onTensile Strength of Thermal Barrier Coatings
Wang Depeng,Li Qinghui,Wang Xudong.Eeffect of Substrate Preheating Temperature onTensile Strength of Thermal Barrier Coatings[J].Aerospace Materials & Technology,2010,40(3).
Authors:Wang Depeng  Li Qinghui  Wang Xudong
Institution:The Second Artillery Qingzhou Petty Officers School
Abstract:ZrO2 coating was developed by plasma spraying process in different substrate preheating temperature, and the tensile test and XRD were used to investigate the influence of substrate preheating temperature on tensile strength. The highest tensile strength can be obtained when the substrate preheating temperature is 250, the highest value is 13.4 MPa.When substrate preheating temperature is higher than 350, the mass of the thermally grown oxide on bond coatings increased more and the tensile strength reduced.
Keywords:Thermal barrier coatings  Plasma spraying  Substrate preheating temperature  Bond strength
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《宇航材料工艺》浏览原始摘要信息
点击此处可从《宇航材料工艺》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号