Gas turbine engine augmentor

Details Gas turbine engine augmentor Gas turbine engine augmentor

F - Mech Eng,Light,Heat,Weapons

02

C

60/174

F02C 1/00 (2006.01) F23R 3/18 (2006.01)

Patent

CA 1281554

Abstract Gas Turbine Engine Augmentor The pilot section of a flameholder of an augmentor for a gas turbine engine is modified to improve the ignition and stability characteristics by judiciously locating aperture(s) or slot(s) in the pilot section wherein their orientation is critical so as to create a vortical flow field.

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