摘要
对航空发动机封严蜂窝组件的钎焊工艺进行了探索、研究,完成了钎焊的溶蚀、钎着率试验,并在试焊模拟件的基础上完成了试生产。
The brazing technology of sealing honeycomb assembly of aeroengine is studied. The tests for dissolve corrosion and ratio of brazing area are accomplished. Trial production is completed on the basis of trial welding.
出处
《航空工艺技术》
1998年第6期36-37,共2页
Aeronautical Manufacturing Technology
关键词
蜂窝组件
溶蚀
钎着率
航空发动机
钎焊
Honeycomb assembly Dissolve corrosion Ratio of brazing area