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US Patent 7584619 System for reducing oil consumption in gas turbine engines

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Patent
Patent
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Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
75846190
Date of Patent
September 8, 2009
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Patent Application Number
117350200
Date Filed
April 13, 2007
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Patent Citations Received
‌
US Patent 11859563 Air system of multi-engine aircraft
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Patent Primary Examiner
‌
William H. Rodriguez
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Patent abstract

A system for reducing oil usage from a sump in a gas turbine engine. Two sources of oil usage, which usage includes leakage and consumption, have been identified: (1) during idle, leakage of oil from an oil sump through seals and (2) during high-power operation, consumption of oil entrained in vent air exiting from the sump. At idle, the invention reduces pressure in the sump, to thereby increase airflow across the seals into the sump, to inhibit the oil leakage across the seals. At high power operation, the pressure reduction is terminated, but flow exiting the vent is artificially restricted.

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