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US Patent 7328098 Determining bleed valve failures in gas turbine engines

Patent 7328098 was granted and assigned to United Technologies on February, 2008 by the United States Patent and Trademark Office.

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Current Assignee
United Technologies
United Technologies
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
7328098
Date of Patent
February 5, 2008
Patent Application Number
11732318
Date Filed
April 3, 2007
Patent Citations Received
‌
US Patent 11859563 Air system of multi-engine aircraft
0
Patent Primary Examiner
‌
Richard M Camby
Patent abstract

The invention detects gas turbine bleed valve position discordances. The invention derives a modified exhaust gas temperature derivative as the predictive criteria in conjunction with a control logic to determine bleed valve position discordances that may indicate a mechanical failure in a valve, or in the control means for a valve.

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