Augmentor pilot nozzle

Details Augmentor pilot nozzle Augmentor pilot nozzle

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 3/10 (2006.01) F23R 3/20 (2006.01)

Patent

CA 2462753

A gas turbine engine augmentor nozzle has an inlet for connection to an augmentor fuel conduit and an outlet for expelling a spray of fuel. A passageway between the inlet and outlet is at least partially bounded by outlet end surface portions diverging from each other. The nozzle may be used as a replacement for a non-divergent nozzle and may reorient a fuel jet centerline toward radial.

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