INTER-COMPRESSOR CROSS-OVER PIPE HEAT EXCHANGER
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United States of America Patent
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Issued Date -
Oct 29, 2020
app pub date -
May 8, 2019
filing date -
Apr 26, 2019
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Abstract
The gas turbine engine described includes a first centrifugal compressor, a second centrifugal compressor, and intercompressor pipes extending therebetween. The intercompressor pipes fluidly interconnect an exit of a first impeller of the first centrifugal compressor and an inlet of a second impeller of the second centrifugal compressor. The intercompressor pipes have heat transfer structures on outer surfaces thereof to increase convective heat transfer.
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