Combustor nozzle

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

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Details

F23R 3/42 (2006.01)

Patent

CA 2569299

A gas turbine engine swirler/nozzle apparatus has a swirler having a central axis and a nozzle. The nozzle has an outlet end with a plurality of outlets about said axis and having an asymmetry about said axis. The apparatus may be formed as a reengineering of a baseline apparatus having a symmetric nozzle.

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