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:
Jan. 23, 2018

Filed:

May. 29, 2013
Applicants:

Clifford Hatcher, Jr., Orlando, FL (US);

Forrest R. Ruhge, Orlando, FL (US);

Inventors:

Clifford Hatcher, Jr., Orlando, FL (US);

Forrest R. Ruhge, Orlando, FL (US);

Assignee:

Siemens Energy, Inc., Orlando, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/02 (2006.01); G01M 15/14 (2006.01); F01D 21/00 (2006.01); F02C 7/047 (2006.01); F02C 7/057 (2006.01); G01J 5/00 (2006.01);
U.S. Cl.
CPC ...
F01D 25/02 (2013.01); F01D 21/003 (2013.01); F02C 7/047 (2013.01); F02C 7/057 (2013.01); G01M 15/14 (2013.01); F05D 2260/80 (2013.01); F05D 2270/44 (2013.01); F05D 2270/804 (2013.01); F05D 2270/8041 (2013.01); G01J 5/0088 (2013.01);
Abstract

Gas turbine inlet guide vane ice detection and control systems and methods that utilize active infra-red monitoring of inlet guide vanes, detection of ice formation on the guide vanes and elimination of the ice by altering properties of the gas turbine inlet intake airflow, such as by introducing compressed and/or heated air bled from the turbine. Ice has lower detectable emissivity intensity in the infra-red spectrum than ice-free inlet guide vane surfaces. Ice formation is inhibited by direct monitoring of inlet guide vane icing conditions, rather than by indirect empirical assumptions of ice formation based on atmospheric condition monitoring. Direct monitoring mitigates ice formation in real time without reliance on excessive use of gas turbine compressed or heated air bleed, which enhances turbine operational efficiency.


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