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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Gas turbine engine anti-ice formation device and system

Invented by: Tina H. Chaney
Phoenix, AZ

Dave G. Dischinger
Tempe, AZ

Alan G. Tiltman
Fountain Hills, AZ

Dwight D. Vettel
Chandler, AZ

Originally Assigned to: Honeywell International Inc.
Morristown, NJ
[Now assigned to . . .]

Issued:2011-01-25
Filed:2007-06-18
Application No:11764581
Examined by:Cuff; Michael

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.

[pdf] U.S. Pat. No. 7,874,137

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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