Gas turbine engine thermal management system
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United States of America Patent
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May 10, 2016
Grant Date -
Aug 8, 2013
app pub date -
Mar 13, 2013
filing date -
Oct 31, 2011
priority date (Note) -
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Abstract
A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger A first sensor senses a first characteristic of a second fluid that is communicated through the heat exchanger to exchange heat with the first fluid and a second sensor senses a second characteristic of the second fluid. A positioning of the valve is based on at least one of the first characteristic and the second characteristic.
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