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    • 3. 发明公开
    • Corrosion coating for turbine blade environmental protection
    • KorrosionsbeschichtungfürUmweltschutz einer Turbinenschaufel
    • EP1820875A2
    • 2007-08-22
    • EP06126889.2
    • 2006-12-21
    • General Electric Company
    • Nagaraj, Bangalore AswathaGorman, Mark Daniel
    • C23C10/04C23C10/18C23C10/26C23C10/28C23C10/52F01D5/28C23C10/60
    • C23C10/04C23C10/18C23C10/26C23C10/28C23C10/52C23C10/60F01D5/288Y10T428/12931
    • A gas turbine engine turbine blade (10) and method for making the same comprising an airfoil section (12), a platform section (14), an under platform section (16), and a dovetail section (18) having an exterior surface (32), the exterior surface of the dovetail section comprising a shank (26) and a serrated exterior (28). The blade (10) further comprises a silicon-modified diffusion aluminide layer a surface of a turbine blade section selected from the group consisting of the exterior surface of the under platform section (32), the exterior surface of the dovetail section (26), and combinations thereof, the silicon modified diffusion aluminide layer having a concentration of silicon at a surface of the silicon-modified diffusion aluminide layer in the range of about 1 weight percent to about 10 weight percent and a concentration of aluminum at the surface of the silicon modified diffusion aluminide layer in the range of about 5 weight percent to about 25 weight percent.
    • 一种燃气涡轮发动机涡轮叶片(10)及其制造方法,包括机翼部分(12),平台部分(14),平台下部分(16)和具有外表面的燕尾部分(18) 32),燕尾部分的外表面包括柄(26)和锯齿状外部(28)。 叶片(10)还包括硅改性的扩散铝化物层,涡轮叶片部分的表面,其选自下平台部分(32)的外表面,燕尾部分(26)的外表面, 硅改性扩散铝化物层在硅改性扩散铝化物层的表面上具有在约1重量%至约10重量%的范围内的硅浓度,硅的表面处的铝的浓度 改性扩散铝化物层的范围为约5重量%至约25重量%。