| 摘要 |
<p>A turbine engine assembly (10) includes a core gas turbine engine (12), a first low-pressure turbine section (80,116,316,416,516) in serial flow communication with the core gas turbine engine, the first low-pressure turbine section configured to rotate in a first rotational direction a first gear assembly (322) coupled to the first low-pressure turbine section, a second low-pressure turbine section (82,118,418,518) coupled to the gear assembly, the second low-pressure turbine section configured to rotate in a second rotational direction, and a fan assembly (124,324,426,524) coupled to the second low-pressure turbine section.</p> |
