Fan cowl support for a turbofan engine

摘要

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. The forward end of the support is pivotally connected to the engine fan case by a plurality of non-vertical forward links.