Invention Grant
US08420238B2 Use of a tungsten bronze structured material and turbine component with a thermal barrier coating 失效
使用具有热障涂层的钨青铜结构材料和涡轮机部件

Use of a tungsten bronze structured material and turbine component with a thermal barrier coating
Abstract:
A tungsten bronze structured ceramic material as a thermal barrier coating is described wherein the tungsten bronze structured ceramic coating material has the formula AO—BvOw—CyOz where O stands for Oxygen, A stands for a 2+ or a 1+ cation, B stands for a 2+ or 3+ cation and C stands for a 4+ or a 5+ cation. The thermal barrier coating may be applied for gas turbine components.
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