| CPC B64C 27/68 (2013.01) [B60L 15/20 (2013.01); B60L 50/60 (2019.02); B64C 27/10 (2013.01); B64C 27/467 (2013.01); B64C 27/605 (2013.01); B64D 17/80 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B60L 2200/10 (2013.01)] | 17 Claims |

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1. A hover-capable aircraft, comprising:
a body;
a first rotor assembly rotatably coupled to the body, wherein the first rotor assembly includes a first plurality of circumferentially-spaced blades and is configured to rotate about a rotational axis in a first rotational direction; and
a second rotor assembly rotatably coupled to the body, wherein the second rotor assembly includes a second plurality of circumferentially-spaced blades and is configured to rotate about the rotational axis in a second rotational direction opposite the first rotational direction;
wherein each blade of at least one of the first plurality of blades and the second plurality of blades comprises a root, a forward swept section extending directly from the root, and a rearward swept section.
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