GAS TURBINE ENGINE COMBUSTOR HEAT EXCHANGER
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United States of America Patent
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Issued Date -
Jan 1, 2015
app pub date -
Dec 17, 2013
filing date -
Feb 23, 2013
priority date (Note) -
Abandoned
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Abstract
A gas turbine engine having a combustor is disclosed in which a heat exchanger is disposed within the combustor. The heat exchanger can take the form of a fuel/air heat exchanger. In one form the heat exchanger includes a path for cooling air to be conveyed to a location external to the combustor. Cooled cooling air carried through the path can be created through action of heat transfer from the cooling air to a fuel flowing in the heat exchanger. The heat exchanger can include a fuel vaporizer in one form.
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