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发明公开
CN105464723A 涡轮机部件以及涡轮机部件涂层方法 无效 - 撤回

涡轮机部件以及涡轮机部件涂层方法
摘要：
本发明涉及一种涡轮机部件以及涡轮机部件涂层方法。所述涡轮机部件包括至少一个流体流动通路和至少一个孔，至少一个孔布置在涡轮机部件的表面上并且流体地连接至至少一个流体流动通路。至少一个孔包括从至少一个流体流动通路延伸至表面的底面；以及布置在底面的内部部分与底面的外部部分之间的台阶，使得底面的内部部分和底面的外部部分不包括单一的平面表面。
摘要（英）：

The present invention relates to a turbine component and a turbine component coating process. Turbine components include at least one fluid flow passage at least one aperture disposed on a surface of the turbine component and fluidly connected to the at least one fluid flow passage. The at least one aperture includes a floor extending from the at least one fluid flow passage to the surface; and, a step disposed between an inner portion of the floor and an outer portion of the floor such that the inner portion of the floor and the outer portion of the floor do not comprise a single planar surface.

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