GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE
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United States of America Patent
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Issued Date -
Sep 27, 2018
app pub date -
Feb 6, 2018
filing date -
Feb 6, 2018
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Abstract
A gas turbine engine includes a core engine defined about an axis, a gear system driven by the core engine, and a pylon variable area flow system. A fan is driven by the gear system. The variable area flow system operates to effect the bypass flow.
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