ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE
卷宗概要
发明人
Gabriel L. Suciu; Brian D. Merry; Christopher M. Dye; Steven B. Johnson; Frederick M. Schwarz
IPC 分类
CPC 分类
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.
原文（中文）
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.