发明名称 |
REVERSE CORE GEAR TURBOFAN |
摘要 |
A gas turbine engine has a fan at an axially outer location. The fan rotates about an axis of rotation. The fan delivers air into an outer bypass duct, and across a booster fan positioned radially inwardly of the outer bypass duct. The booster fan delivers air into a radially middle duct, and across a cold turbine into a radially inner core duct being directed into a compressor. From the compressor, air flows axially in a direction back toward the fan through a combustor section, and across an exhaust of the turbine section as directed into the middle duct. A gear reduction drives the fan from a fan drive turbine section. A method is also disclosed. |
申请公布号 |
US2013255224(A1) |
申请公布日期 |
2013.10.03 |
申请号 |
US201213431048 |
申请日期 |
2012.03.27 |
申请人 |
KUPRATIS DANIEL BERNARD;MOON FRANCIS R. |
发明人 |
KUPRATIS DANIEL BERNARD;MOON FRANCIS R. |
分类号 |
F02K3/065;F02C3/06;F02C3/107 |
主分类号 |
F02K3/065 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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