Methods and apparatus for washing gas turbine engine combustors

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/00 (2006.01) B08B 9/032 (2006.01) F23D 11/38 (2006.01) F23R 3/00 (2006.01)

Patent

CA 2457970

A method facilitates washing a gas turbine engine combustor. The method comprises coupling a nozzle assembly against the combustor, wherein the nozzle assembly includes an inlet end, a discharge end, a hollow nozzle body extending therebetween, and a centerbody positioned within the nozzle body, coupling the nozzle assembly to a fluid source, and discharging an annulus of fluid from the nozzle assembly into the combustor to facilitate removing particulate matter from the combustor.

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