| 摘要 |
A turbofan engine assembly (10) including a booster compressor (30) coupled to an upstream end of a core gas turbine engine (12), an intermediate- pressure turbine (32) coupled to the booster compressor, the intermediate-pressure turbine disposed downstream from the core gas turbine engine, a first fan assembly (50) coupled to a low-pressure turbine (14), a second fan assembly (52) disposed downstream from the first fan assembly, and a gearbox (100) coupled between the second fan assembly and the low-pressure turbine. |
