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. 25, 2011

Filed:

Jun. 18, 2007
Applicants:

Tina H. Chaney, Phoenix, AZ (US);

Dave G. Dischinger, Tempe, AZ (US);

Alan G. Tiltman, Fountain Hills, AZ (US);

Dwight D. Vettel, Chandler, AZ (US);

Inventors:

Tina H. Chaney, Phoenix, AZ (US);

Dave G. Dischinger, Tempe, AZ (US);

Alan G. Tiltman, Fountain Hills, AZ (US);

Dwight D. Vettel, Chandler, AZ (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02G 3/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

An anti-ice formation device for a gas turbine engine is configured to be mounted within an inlet duct of the engine, and adjacent the gas turbine engine compressor inlet. The device is configured to selectively receive a flow of compressed air that is discharged from the compressor. Because the compressed air is relatively hot, the anti-ice formation device temperature increases to a temperature sufficient to prevent ice accumulation and formation in the engine inlet duct. The anti-ice formation device is also configured such that heat is not transferred to the compressor inlet housing. As a result, the anti-ice formation device does not cause impeller clearance variations, which would adversely affect engine performance.


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