Fluted chevron exhaust nozzle

Power plants – Reaction motor – Air passage bypasses combustion chamber

Reexamination Certificate

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Details

C060S770000

Reexamination Certificate

active

07963099

ABSTRACT:
A gas turbine engine exhaust nozzle includes a fluted shell terminating in a row of chevrons. The nozzle is radially serpentine circumferentially around the shell and has a circumferentially serpentine trailing edge.

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