Augmentor

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F - Mech Eng,Light,Heat,Weapons

02

K

F02K 3/10 (2006.01) F23D 14/74 (2006.01) F23R 3/34 (2006.01)

Patent

CA 2458280

A turbine engine has a centerbody within a gas flowpath and a downstream tailcone and a pilot at an upstream end of the tailcone. A flameholder is positioned in the flowpath outboard of the centerbody. The pilot has a first surface diverging in a downstream direction.

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