Invention Grant
- Patent Title: Method and system for determining gas turbine tip clearance
- Patent Title (中): 确定燃气轮机顶端间隙的方法和系统
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Application No.: US13692791Application Date: 2012-12-03
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Publication No.: US08827630B2Publication Date: 2014-09-09
- Inventor: Tonghuo Shang , Anthony D. Kurtz
- Applicant: Kulite Semiconductor Products, Inc.
- Applicant Address: US NJ Leonia
- Assignee: Kulite Semiconductor Products, Inc.
- Current Assignee: Kulite Semiconductor Products, Inc.
- Current Assignee Address: US NJ Leonia
- Agency: Troutman Sanders LLP
- Agent James E. Schutz
- Main IPC: F01D25/00
- IPC: F01D25/00

Abstract:
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.
Public/Granted literature
- US20130091940A1 Method and System for Determining Gas Turbine Tip Clearance Public/Granted day:2013-04-18
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