Fluidic vectoring for exhaust nozzle
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United States of America Patent
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Jan 17, 2012
Grant Date -
Dec 4, 2008
app pub date -
May 31, 2007
filing date -
May 31, 2007
priority date (Note) -
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Abstract
An exhaust nozzle assembly provides fluidic thrust vectoring of the primary stream to enhance aircraft maneuverability. The exhaust nozzle assembly includes a cooling air passage that supplies cooling air. A vector opening injects cooling airflow into the exhaust passage to the primary stream. A cover plate is movable to partially block the vector openings and adjust the location of injection of the cooling airflow into the exhaust passage.
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