Gas turbine engine premix injectors

Details Gas turbine engine premix injectors Gas turbine engine premix injectors

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/28 (2006.01) F02C 7/22 (2006.01)

Patent

CA 2630721

One embodiment is a gas turbine engine premix injector including a mixing duct, a plurality of air inlet slots leading to the duct, a plurality of gaseous fuel inlet apertures leading to the duct, a plurality of vanes positioned in the duct downstream from said air inlets, a plurality of liquid fuel inlet apertures leading to the duct, and a plurality of discharge windows positioned between the vanes.

Un mode de réalisation est un injecteur de prémélange de turbine à gaz comprenant un conduit de mélange, une pluralité de fentes d'entrée d'air menant au conduit, une pluralité d'ouvertures d'entrée de combustible gazeux menant au conduit, une pluralité d'ailettes disposées dans le conduit en aval des entrées d'air, une pluralité d'ouvertures d'entrée de combustible liquide menant au conduit, ainsi qu'une pluralité de fenêtres d'évacuation disposées entre les ailettes.

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