Invention Grant
US08151551B2 Variable area fan nozzle thrust reverser 有权
可变区域风扇喷嘴推力反向器

Variable area fan nozzle thrust reverser
Abstract:
A nozzle for use in a gas turbine engine includes nozzle doors coupled with a fan nacelle wherein the nozzle doors move in unison between a plurality of positions to influence a bypass airflow through a fan bypass passage. A linkage connects the nozzle doors and an actuator. A louver section coupled with the linkage moves in unison with the nozzle doors between a plurality of louver positions to direct a portion of the bypass airflow in a selected direction.
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