Gas turbine engine heat exchanger system
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United States of America Patent
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Mar 13, 2018
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N/A
app pub date -
Dec 12, 2013
filing date -
Mar 5, 2013
priority date (Note) -
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Abstract
An apparatus includes a gas turbine engine and a heat transfer system. The gas turbine engine includes an inlet particle separator that separates inlet air into scavenge air and clean air. A scavenge air path conveys the scavenge air from the inlet particle separator to the heat transfer system. A heat exchange fluid path conveys a heat exchange fluid to the heat transfer system and a cooled heat exchange fluid away from the heat transfer system. The heat transfer system is configured to transfer heat from the heat exchange fluid path to the scavenge air path to cool the heat exchange fluid.
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