Power plants – Reaction motor – Air passage bypasses combustion chamber
Reexamination Certificate
2007-12-11
2007-12-11
Rodriguez, William H. (Department: 3746)
Power plants
Reaction motor
Air passage bypasses combustion chamber
C060S226100
Reexamination Certificate
active
10774963
ABSTRACT:
A gas turbine engine exhaust nozzle includes a row of laterally sinuous chevrons extending from an aft end of an exhaust duct. The chevrons have radially outer and inner surfaces bound by a laterally sinuous trailing edge extending between a base of the chevrons adjoining the duct and an axially opposite apex of the chevrons. Each chevron has a compound arcuate contour both axially and laterally, and the sinuous trailing edge of the chevrons further compounds the arcuate configuration of each chevron.
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Bailey William Andrew
Blodgett Keith Edward James
Early Kevin Sean
Martens Steven
Price Kenneth Daniel
Andes William S.
Conte Francis L.
Rodriguez William H.
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