Invention Grant
US08739515B2 Variable area fan nozzle cowl airfoil 有权
可变区域风扇喷头罩面翼型

Variable area fan nozzle cowl airfoil
Abstract:
A nacelle assembly for a high-bypass gas turbine engine includes a variable area fan nozzle having a first fan nacelle section and a second fan nacelle section. The second fan nacelle section being axially movable relative the first fan nacelle section to define an auxiliary port to vary a fan nozzle exit area and adjust fan bypass airflow, the second fan nacelle section includes at least one cowl with an inner portion, an outer portion and a multiple of stiffeners therebetween to increase a flutter margin.
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