燃烧
材料科学
点火系统
航空航天
航空发动机
表征(材料科学)
气体压缩机
自燃温度
冶金
热力学
机械工程
纳米技术
航空航天工程
化学
物理化学
工程类
物理
作者
Lei Shao,Wensheng Li,Dongyue Li,Guoliang Xie,Chunzhi Zhang,Cheng Zhang,Jinfeng Huang
标识
DOI:10.1016/j.jallcom.2023.170584
摘要
Ti alloys are widely used in aero-engines due to their excellent comprehensive performance. However, Ti alloys show ignition sensitivity, which is attributed to their poor heat conductivity, high oxidation heat and active chemical performance, especially in high-pressure compressors. This paper summarizes the combustion characteristics and mechanisms of Ti alloys. The thermodynamic conditions and physical models of Ti alloys combustion are established. The nature, characterization parameters and influencing factors of the combustion threshold are clarified. Several commonly used methods of the burn resistant property are introduced. Furthermore, the development tendency is prospected for improving Ti alloys safety services in aerospace.
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