Invention Grant
US07712313B2 Fuel nozzle for a gas turbine engine 有权
用于燃气轮机的燃油喷嘴

Fuel nozzle for a gas turbine engine
Abstract:
In the fuel nozzle, the fuel is circulated in a helical path around the interface of a stem of the fuel nozzle and a flange for increase the cooling.
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