Flow path routing within a gas turbine engine
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United States of America Patent
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Mar 6, 2018
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app pub date -
Sep 18, 2014
filing date -
Sep 20, 2013
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Abstract
An example gas turbine engine with multiple flow paths includes, among other things, a core flow path extending from a compressor section to an exhaust section, a bypass duct providing a bypass flow path radially outside the core flow path, and a flow injection device to selectively communicate a first amount of flow or a second amount of flow from the bypass flow path to the exhaust section, the first amount of flow different than the second amount of flow.
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