Invention Grant
US08398018B2 Fan cowl support for a turbo fan engine 有权
风扇罩支持涡轮风扇发动机

Fan cowl support for a turbo fan engine
Abstract:
A fan cowl support for an aircraft having an engine pylon, an engine fan case and an engine fan cowl. The fan cowl support includes a support having a forward end connected to the engine fan case and an aft end connected to the engine pylon with a spherical connector. At least a portion of the engine fan cowl is connected to the support.
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