战略航空航天应用的耐高温涂层

Pub Date : 2023-03-09 DOI:10.14429/dsj.73.18638
Zafir Alam, Chandrakant Parlikar, Mahesh Kumawat, S. Gokul Lakshmi, Dipak Das
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引用次数: 0

摘要

在航空发动机和燃烧室的热段运行的航空部件经历极端环境。通常,这些部件要经受超过1100℃的高温和氧化条件。保护涂层对于防止氧化引起的部件尺寸退化,增强其高温性能和耐久性至关重要。国防冶金研究实验室(DMRL)已经开发了多种金属和陶瓷热障涂层(TBC)系统,用于镍基高温合金和难熔铌合金,用于涉及超高温和高流速的战略航空航天应用。这些涂层已经证明了在静态空气氧化过程中,在高达2000℃的温度下,以及在涉及高流速(马赫>本文综述了DMRL开发的高级抗氧化和热障涂层。在实验室规模上评估了tbc在防止金属和复合衬底材料尺寸退化方面的有效性。所研制的tbc具有应用于航空发动机和超高速飞行器推进系统的潜力。
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High Temperature Resistant Coatings for Strategic Aero space Applications
The aerospace components operating in hot sections of aero-engines and combustors experience extreme environments. Typically, the components are subjected to high service temperatures exceeding 1100°C and oxidizing conditions. Protective coatings are essential for preventing oxidation-induced dimensional degradation of the components and enhancing their high temperature capability as well as durability. Defence Metallurgical Research Laboratory (DMRL) has developed a variety of metallic and ceramic thermal barrier coating (TBC) systems for Ni-base superalloys, and refractory Nb-alloys for strategic aerospace applications involving ultra-high temperatures and high flow velocities. These coatings have demonstrated significant effectiveness against thermal degradation at temperatures as high as 2000 °C during oxidation in static air as well as in dynamic conditions involving high flow velocities (Mach > 2). The present article provides an overview of the advanced oxidation resistant and thermal barrier coatings developed in DMRL. The effectiveness of the TBCs in preventing dimensional degradation of the metallic and composite substrate materials has been evaluated at the laboratory scale. The developed TBCs have the potential for use in aero-engines and propulsion systems of hypervelocity vehicles.
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