| 摘要 |
An aircraft with a fuselage and two aerodynamic wings, which each accommodate at least two propeller drives spaced a apart from each other in the wingspan direction, each with a propeller rotational axis, wherein the aircraft has a controller for activating the propeller drives, wherein in one operating mode of the controller for generating propulsion, the propeller drives are activated in such a way that the outer section of a propeller secured to the respective propeller rotational axis is moved from the top down on the side facing the fuselage.
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