Invention Grant
US08176725B2 Reversed-flow core for a turbofan with a fan drive gear system 有权
具有风扇驱动齿轮系统的涡轮风扇的反流芯

Reversed-flow core for a turbofan with a fan drive gear system
Abstract:
A gas turbine engine comprises a fan drive gear system, a low spool connected to the fan drive gear system, and a high spool disposed aft of the low spool. The low spool comprises a rearward-flow low pressure compressor disposed aft of the fan drive gear system, and a forward-flow low pressure turbine disposed aft of the low pressure compressor. The high spool comprises a forward-flow high pressure turbine disposed aft of the low pressure turbine, a combustor disposed aft of the high pressure turbine, and a forward-flow high pressure compressor disposed aft of the combustor.
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