Invention Application
US20090050714A1 FUEL NOZZLE FOR A GAS TURBINE ENGINE 有权
燃气喷嘴用于燃气涡轮发动机

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.
Public/Granted literature
Information query
Patent Agency Ranking
0/0