高温涂层的广泛使用在很大程度上拓展了高温合金的应用领域,但随着航空发动机用涡轮叶片服役环境的日益苛刻,合理评价涂层/高温合金体系综合性能,尤其热机械疲劳、蠕变疲劳等性能备受关注.该体系综合性能的评价必然涉及到与高温涂层材料本身相关的物理、化学、力学等性能.本文将对近年来有关高温涂层材料的物理和力学等方面的性能进行综述,并据此探讨今后涂层/基体界面行为研究的新思路.
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