Nozzle assembly with flow conduits
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United States of America Patent
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Dec 4, 2012
Grant Date -
May 7, 2009
app pub date -
Nov 1, 2007
filing date -
Nov 1, 2007
priority date (Note) -
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Abstract
A nozzle assembly for a turbine engine has a convergent portion for converging fluid flow from a turbine engine core. A divergent portion for diverging fluid flow from the turbine engine core is in fluid communication with the convergent portion. A conduit is in communication with a bypass fluid flow. The conduit has a thrust vectoring port located near the divergent portion.
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