ANGLED REVERSE CORE GAS TURBINE ENGINE WITH WIDENED NOZZLE
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United States of America Patent
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Issued Date -
Aug 27, 2015
app pub date -
Apr 30, 2014
filing date -
Feb 25, 2014
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Abstract
A propulsion system for an aircraft includes a furcated nozzle that has at least a first duct that extends from a first propulsor to a first trailing end duct opening and a second duct that extends from a second propulsor to a second trailing end duct opening.
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