RECUPERATOR FOR GAS TURBINE ENGINES
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United States of America Patent
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Issued Date -
Jun 23, 2011
app pub date -
Dec 31, 2009
filing date -
Dec 31, 2008
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
A recuperator for use in transferring heat from gas turbine exhaust gases to compressed air inlet gases before combustion. The recuperator utilizes a plurality of stacked foils that define microchannels to form a recuperator having high effectiveness and low pressure drop while maintaining a low weight. Accordingly, the recuperator presented herein may be incorporated into light aircraft and helicopters without significantly compromising the performance thereof.
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