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Patent

Ducted fan engine exhaust mixer

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TLDR
In a turbofan engine, the turbine exhaust gas is directed to a number of circumferentially spaced exhausts, the outlets of which are inclined to the axis of the engine as discussed by the authors.
Abstract
A turbofan engine has an exhaust arrangement for the bypassed air and turbine exhaust gases providing for mixing of the two before a common propulsion nozzle. The turbine exhaust gas is directed to a number of circumferentially spaced exhausts, the outlets of which are inclined to the axis of the engine. A baffle extending from the end of the bypass duct into the common exhaust duct divides the bypass air into a portion inside and a portion outside of the baffle, the former mixing initially with the turbine exhaust gases and the resulting mixture then being mixed with the remainder of the bypass air. The baffle includes lobes which extend downstream and inwardly so as to obscure the outlets of the turbine exhaust from the jet nozzle, thus minimizing thermal radiation through the nozzle.

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Gas turbine by-pass engine

TL;DR: A gas turbine bypass jet engine comprises a bypass duct also an ancillary air duct each of which is arranged to receive air compressed by the engine compressor, there being conduit means for introducing air from the by-pass duct into the jet pipe to mix with the turbine exhaust gases therein this article.