科技报告详细信息
Fatigue Behavior of Coated Titanium Alloys
Zhu, Dongming ; Lerch, Bradley A ; Kalluri, Sreeramesh
关键词: ALUMINUM ALLOYS;    BARRIER LAYERS;    COATINGS;    CORROSION RESISTANCE;    CRACK INITIATION;    CRACK PROPAGATION;    DUCTILITY;    DURABILITY;    EROSION;    FATIGUE LIFE;    NITRIDES;    OXIDATION RESISTANCE;    TITANIUM ALLOYS;   
RP-ID  :  NASA/TM-2019-219999,E-19607,GRC-E-DAA-TN61136
学科分类:金属与冶金
美国|英语
来源: NASA Technical Reports Server
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【 摘 要 】

Advanced multi-component TiAlCrTaSiN-based multilayered coatings were developed and processed onto Ti-6Al-4V (Ti-6-4) and GammaMet PX (GMPX or TiAl) alloys by a magnetron-enhanced physical vapor deposition technique. The coatings have recently been in development with the goal of improving advanced titanium alloy, turbine engine component durability and oxidation-erosion resistance. In this work, the performance of the multi-component coating system (including the outer layer nitride based coating and inner TiAlCrSi oxidation barrier bond coat) was studied, and the coating's influence on the fatigue behavior of the titanium-based alloys were compared. Although the multi-component coating was initially optimized to improve the coating's high temperature oxidation and erosion resistance, the lower ductility nitride-based coating needs further work on microstructure or composition to improve its mechanical stress resistance and strain tolerance for use in cyclically loaded, turbine blade operating conditions. This is particularly true for GMPX and other γ-TiAl alloys because these intermetallic titanium alloys have limited ductility and are very sensitive to defects such as coating cracks. However, the inner layer TiAlCrSi-coating had better adhesion and ductility, and may be a suitable choice to improve the oxidation resistance of titanium alloys.

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