SYSTEM AND METHOD FOR OPERATING A PRECOOLER IN AN AIRCRAFT
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United States of America Patent
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Mar 13, 2017
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Mar 17, 2011
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Abstract
A method for controlling a pressure control mechanism in a turbofan engine having a precooler permitting heat exchange between ambient air and bleed air includes detecting at least one of an engine failure or a bleed system failure, detecting at least one of an ice condition or an activation of an anti-ice system, and actuating the pressure control mechanism, thereby altering the heat exchange between the ambient air and the bleed air.
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