Invention Grant
US08839806B2 Pressure tap assembly for turbine system and method for assembly of a pressure tap assembly 有权
用于涡轮机系统的压力分接头组件和用于组装压力分接组件的方法

Pressure tap assembly for turbine system and method for assembly of a pressure tap assembly
Abstract:
According to one aspect of the invention, a pressure tap assembly includes a passage formed through a wall, a counterbore formed in the passage proximate an inner surface of the wall and a first end of a tube positioned in the passage, wherein a spacer positioned on the tube is positioned in the counterbore and deformed about the inner surface and counterbore to prevent fluid flow between the passage and tube. The pressure tap assembly also includes a second end of the tube disposed proximate a pressure sensing device.
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