Three-stream gas turbine engine architecture
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United States of America Patent
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Apr 24, 2018
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app pub date -
Oct 21, 2014
filing date -
Oct 21, 2014
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Abstract
A gas turbine engine includes an auxiliary airflow control system to provide selective communication of a portion of a second stream from a second stream flow path into a third stream flow path, the auxiliary airflow control system in communication with a high temperature flow sourced from the turbine section.
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