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DOE OSTI · 2542506

Bypass heat exchanger configuration to reroute core flow

Terwilliger, Neil
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Abstract

A turbine engine assembly includes a heat exchanger that is in thermal communication with an exhaust gas flow. A bypass passage is provided that is configured to selectively route at least a portion of the exhaust gas flow around the heat exchanger in response to a predefined engine operating condition.

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BibTeXRIS

Terwilliger, Neil. 2024-08-20. Bypass heat exchanger configuration to reroute core flow. https://www.osti.gov/biblio/2542506

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