The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 24, 2009

Filed:

Sep. 30, 2005
Applicants:

Onder Uluyol, Fridley, MN (US);

Kyusung Kim, Plymouth, MN (US);

Charles M. Ball, Gilbert, AZ (US);

Inventors:

Onder Uluyol, Fridley, MN (US);

Kyusung Kim, Plymouth, MN (US);

Charles M. Ball, Gilbert, AZ (US);

Assignee:

Honeywell International, Inc., Morristown, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/26 (2006.01); F02C 7/22 (2006.01); F01N 3/00 (2006.01); F02B 5/00 (2006.01); F02M 51/00 (2006.01); G06F 19/00 (2006.01); G06F 11/30 (2006.01); G06F 15/00 (2006.01); G06G 7/70 (2006.01); G21C 17/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A system and method is provided for startup characterization in a turbine engine that provides the ability to accurately characterize engine startup. The startup characterization system and method uses engine temperature sensor data and engine speed sensor data to accurately characterize the startup of the turbine engine by determining when several key engine startup conditions are reached. By storing and analyzing engine sensor data taken during these key conditions of engine startup, the system and method is able to accurately characterize the performance of the engine during startup. This information can be used as part of a trending system to determine when faults in the start transient regime are occurring or likely to occur. Additionally, this information can be used in real time by control systems to better control the startup and operation of the turbine engine.


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