| 摘要 |
A thrust reverser system (20) deployable from a core cowl (30) is provided. The thrust reverser system (20) may comprise one or more doors (22; 22-1 to 22-7) that are configured to overlap to reduce leakage and increase reverse thrust while deployed. The doors (22; 22-1 to 22-7) may be configured to have vanes (26) that are configured to split and/or direct airflow. |
