Turbofan with variable bypass flow
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United States of America Patent
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Sep 12, 2017
Grant Date -
May 14, 2015
app pub date -
Mar 6, 2014
filing date -
Mar 7, 2013
priority date (Note) -
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Abstract
A gas turbine engine is disclosed with a bypass flow path having a bypass nozzle positioned downstream of a fan; a core flow path having a compressor, a combustor, a turbine and an exhaust nozzle; an auxiliary duct fluidly connecting the core flow path and the bypass flow path downstream of the turbine; and a control valve operably connected to the auxiliary duct to control fluid flow from the core flow path into the bypass flow path.
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