发明名称 |
TURBOFAN ENGINE ASSEMBLY AND METHOD OF ASSEMBLING SAME |
摘要 |
A turbofan engine assembly (10) is provided. The turbofan engine assembly (10) includes a core gas turbine engine (13) including a high-pressure compressor (14), a combustor downstream from the high-pressure compressor, and a high-pressure turbine (18) downstream from the compressor, the high-pressure turbine coupled to the high-pressure compressor. The turbofan engine assembly (10) further includes a first fan assembly (50) coupled within the turbofan engine assembly and located upstream from the core gas turbine engine. The turbofan engine assembly (10) further includes a first gearbox (100) coupled to the first fan assembly. The turbofan engine assembly (10) a booster compressor (22) coupled within the turbofan engine assembly and located downstream from the first fan assembly. The turbofan engine assembly (10) a second gearbox (102) coupled to the booster compressor such that the booster compressor rotates in a rotational direction that is opposite to the rotational direction of the first fan assembly. |
申请公布号 |
CA2612031(C) |
申请公布日期 |
2015.06.16 |
申请号 |
CA20072612031 |
申请日期 |
2007.11.22 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SCHILLING, JAN CHRISTOPHER |
分类号 |
F02C7/36;F02C3/107;F02K3/072 |
主分类号 |
F02C7/36 |
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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