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
-
Application No.: US12387078Application Date: 2009-04-28
-
Publication No.: US07922441B2Publication Date: 2011-04-12
- Inventor: Tonghuo Shang , Anthony D. Kurtz
- Applicant: Tonghuo Shang , Anthony D. Kurtz
- Applicant Address: US NJ Leonia
- Assignee: Kulite Semiconductors Products, Inc.
- Current Assignee: Kulite Semiconductors Products, Inc.
- Current Assignee Address: US NJ Leonia
- Agent James E. Schutz, Esq.; Dean Y. Shahriari; Troutman Sanders LLP
- 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
- US20090280002A1 Method and system for determining gas turbine tip clearance Public/Granted day:2009-11-12
Information query