Flow path routing within a gas turbine engine
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United States of America Patent
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Aug 13, 2019
Grant Date -
Jul 12, 2018
app pub date -
Jan 8, 2018
filing date -
Sep 20, 2013
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Abstract
A method of communicating flow through a gas turbine engine having multiple flow paths according to an exemplary embodiment of the present disclosure includes moving core flow along a core flow path from a compressor section to an exhaust section, selectively communicating a first amount of bypass flow from a bypass flow path defined by a bypass duct to the exhaust section or a second amount of bypass flow from the bypass flow path to the exhaust section, the first amount different than the second amount.
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