- 专利标题: Method and system for determining gas turbine tip clearance
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申请号: US12387078申请日: 2009-04-28
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公开(公告)号: US20090280002A1公开(公告)日: 2009-11-12
- 发明人: Tonghuo Shang , Anthony D. Kurtz
- 申请人: Tonghuo Shang , Anthony D. Kurtz
- 申请人地址: US NJ Leonia
- 专利权人: Kulite Semiconductor Products, Inc.
- 当前专利权人: Kulite Semiconductor Products, Inc.
- 当前专利权人地址: US NJ Leonia
- 主分类号: F01D11/18
- IPC分类号: F01D11/18 ; F01D25/00
摘要:
A system for sensing at least one physical characteristic associated with an engine including a turbine having a plurality of blades turning inside a casing, the system including: a pressure sensor coupled substantially adjacent to the casing and including at least one output; a port in the turbine casing for communicating a pressure indicative of a clearance between the blades and casing to the pressure sensor; a cooling cavity substantially surrounding the pressure sensor; and, an inlet for receiving fluid from the engine and feeding the fluid to the cooling cavity to cool the pressure sensor; wherein, the pressure sensor output is indicative of the clearance between the blades and casing.
公开/授权文献
- US07922441B2 Method and system for determining gas turbine tip clearance 公开/授权日:2011-04-12
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