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Thermal Oxidation Behavior of TiAlCrSiN and AlCrTiN Films on HastelloyX

机译:TiAlcrsin和Alcrtin薄膜在Hastelloyx上的热氧化行为

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In this paper, the thermal oxidation behavior of TiAlCrSiN and AlCrTiN films coated on hastelloyX substrate, typically used for fuel nozzle in gas turbine engine application, have been studied. The thermal oxidation behavior at 950, 1050 and 1150 °C in controlled atmosphere were investigated. The surface appearance, microstructure, chemical composition and adhesion of films were investigated. The thermal oxidations were observed in all testing conditions showing oxide films at the surface with thicker oxide film at higher temperature. However, spalling of oxide scales was found in both coated and uncoated specimens at 1150°C suggesting the maximum working temperature of < 1150 °C for turbine engine applications. The critical loads corresponding to the full delamination of the thermal oxidation coated specimens were found to be higher than the non-thermal oxidation specimens. The effect of thermal oxidation on damage patterns during scratch tests, i.e. less chipping and cracking for thermal oxidation specimen, were also observed.
机译:在本文中,研究了涂覆在摇滚织物基板上的Tialcrsin和铝蛋白膜的热氧化行为,通常用于燃气涡轮发动机应用中的燃料喷嘴。研究了受控气氛中950,1050和1150℃的热氧化行为。研究了表面外观,微观结构,化学成分和薄膜的粘附性。在所有测试条件下观察到热氧化,在较高温度下在表面上显示氧化膜的氧化膜。然而,在1150°C的涂覆和未涂层标本中发现氧化物鳞片的剥落,表明涡轮发动机应用为<1150℃的最大工作温度。发现对应于热氧化涂层标本的完全分层的临界载荷高于非热氧化试样。还观察到热氧化对划痕试验期间损伤模式的影响,即热氧化样品的碎裂较少。

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