| 摘要 |
The invention relates to a rigid wing flying craft having at least one airfoil and at least one driving unit and a cabin for receiving loads. At least one air channel piercing the airfoil is provided in the surface center of the airfoil and at least two steering fins for steering the flight movements are pivotably supported in the air channel. The driving unit and the steering fins are arranged at least partially within said air channel and pivotably supported within the same around an axis of rotation which extends essentially vertically in relation to the axis of the driving unit. |
