Infrared suppressor apparatus and method

Power plants – Reaction motor – Particular exhaust nozzle feature

Reexamination Certificate

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C060S039500, C239S265170

Reexamination Certificate

active

07607306

ABSTRACT:
A method for suppressing infrared radiation from an engine of an aircraft operating in an environment includes directing hot exhaust from the aircraft engine into a lobed mixer of a single baffle infrared suppressor having a collapsible, translatable baffle to generate alternating flows of hot exhaust gas and cold air. The method further includes directing the alternating flows of hot exhaust gas and cold air towards the single baffle assembly to mix the hot exhaust gas with the cold air.

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