发明申请
US20090199561A1 Fuel nozzle for a gas turbine engine and method for fabricating the same 有权
燃气涡轮发动机的燃料喷嘴及其制造方法

Fuel nozzle for a gas turbine engine and method for fabricating the same
摘要:
A method for fabricating a secondary fuel nozzle assembly includes providing a nozzle portion defining a passageway configured to supply fuel. At least one peg is operatively coupled in fuel flow communication with the passageway. The at least one peg extends radially outward from the nozzle portion and defines at least one opening configured to direct a flow of fuel in a substantially upstream direction. A disc is positioned about the nozzle portion upstream of the at least one peg. The disc is positioned in communication with the at least one opening and configured to interfere with the flow of fuel to facilitate fuel atomization.
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