| 摘要 |
A turbine engine assembly (10) is provided. A turbine engine assembly (10) includes a core gas turbine engine (12) includes a high-pressure compressor (18), a combustor (20), and a high-pressure turbine (22). A turbine engine assembly (10) further includes a booster compressor (30) coupled upstream from the core ga s turbine engine. A turbine engine assembly (10) further includes an intermediate- pressure turbine (32) coupled to the booster compressor, the intermediate-pressure turbine disposed downstream from the core gas turbine engine. A turbine engine assembly (10) further includes a counter-rotating fan assembly (16) disposed upstream from the booster compressor, the counter-rotating fan assembly includes a first fan assembly (50) configured to rotate in a first direction and a second fan assembly (52 ) configured to rotate in an opposite second direction. A turbine engine assembly (10) further includes a low-pressure turbine (14) disposed downstream from the intermedia te- pressure turbine, the low-pressure turbine configured to drive the counter- rotating fan assembly. |
