Method and System for Determining Gas Turbine Tip Clearance
AssigneeKulite Semiconductor Products, Inc.
InventorsTonghuo Shang, Anthony D. Kurtz
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AssigneeKulite Semiconductor Products, Inc.
InventorsTonghuo Shang, Anthony D. Kurtz
Estimating the term…
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.
A system for accurately determining blade tip clearance, comprising:
A method for determining turbine blade clearance in a turbomachine having a plurality of radially extending blades within a stationary turbine casing, the method comprising:
A computer-readable medium that stores instructions that, when executed by at least one processor in a system, cause the system to perform a method comprising:
Dependencies are inferred from the claim text.