发明名称 |
EFFICIENT, LOW PRESSURE RATIO PROPULSOR FOR GAS TURBINE ENGINES |
摘要 |
A gas turbine engine includes a spool, a turbine coupled to drive the spool, and a propulsor that is coupled to be driven by the turbine through the spool. A gear assembly is coupled between the propulsor and the spool such that rotation of the turbine drives the propulsor at a different speed than the spool. The propulsor includes a hub and a row of propulsor blades that extends from the hub. The row includes no more than 20 of the propulsor blades. |
申请公布号 |
US2013008146(A1) |
申请公布日期 |
2013.01.10 |
申请号 |
US201113176365 |
申请日期 |
2011.07.05 |
申请人 |
GALLAGHER EDWARD J.;MONZON BYRON R. |
发明人 |
GALLAGHER EDWARD J.;MONZON BYRON R. |
分类号 |
F02K3/075;F01D5/14 |
主分类号 |
F02K3/075 |
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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