| 摘要 |
<p>In a lightweight aircraft having a principal longitudinal load-carrying member, a wing structure mounted on a load-carrying member, a tail rudder and elevator assembly mounted on the load-carrying member, a propeller mounted on the load-carrying member for rotation about the member's longitudinal center line, an engine mounted on the load-carrying member, and a drive transmission dirvingly connecting the engine to the propeller.</p> |
