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Nacelle assembly for a gas turbine engine comprising a pylon located in the fan bypass flow path with a variable area flow system
Nacelle assembly for a gas turbine engine comprising a pylon located in the fan bypass flow path with a variable area flow system
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机译:用于燃气涡轮发动机的机舱组件,包括位于风扇旁路流路中的挂架,该挂架具有可变面积流系统
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摘要
A turbofan engine pylon structure having a fan variable area nozzle defined by a variable area flow system between a pylon intake and a pylon exhaust to selectively adjust a bypass flow. The variable area flow system changes the physical area and geometry of a fan nozzle exit area to manipulate the bypass flow by opening and closing an additional flow area of the variable area flow system.
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