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
- Patent Title: Pressure tap assembly for turbine system and method for assembly of a pressure tap assembly
- Patent Title (中): 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
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Application No.: US13420930Application Date: 2012-03-15
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Publication No.: US08839806B2Publication Date: 2014-09-23
- Inventor: Fredrick Levi Fuller , Wayne Armond Deyoe , Lawrence James Moore
- Applicant: Fredrick Levi Fuller , Wayne Armond Deyoe , Lawrence James Moore
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Cantor Colburn LLP
- Main IPC: F16L55/18
- IPC: F16L55/18 ; B23P17/04

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.
Public/Granted literature
- US20130240054A1 PRESSURE TAP ASSEMBLY FOR TURBINE SYSTEM AND METHOD FOR ASSEMBLY OF A PRESSURE TAP ASSEMBLY Public/Granted day:2013-09-19
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