ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

原文（中国語）

A gas turbine engine may include propulsor means for providing propulsion, reduction means for reducing a rotational speed of an output that drives the propulsor means relative to an input, and expansion means for driving the input of the reduction means. Static support means may support a bearing system that rotatably supports the expansion means and the propulsor means. The support means may support a forward engine mount at a first engine mount location axially near the reduction means relative to an engine axis when the engine is mounted. The support means may support an aft engine mount at a second engine mount location.