CPC B64C 29/0033 (2013.01) [B60L 50/64 (2019.02); B60L 53/00 (2019.02); B64C 13/48 (2013.01); B64C 27/82 (2013.01); B64C 39/12 (2013.01); B64D 27/02 (2013.01); B64D 27/24 (2013.01); B64D 27/40 (2024.01); B64D 31/06 (2013.01); G05D 1/101 (2013.01); B60L 2200/10 (2013.01); B64C 2027/8209 (2013.01); B64D 27/026 (2024.01); B64D 27/402 (2024.01)] | 16 Claims |
1. A vertical takeoff and landing (VTOL) vehicle, including:
a cruise-only propeller;
a hover-and-transition-only tiltrotor;
a first power source that includes an internal combustion engine; and
a second power source that includes a high discharge rate battery and a high energy battery; wherein:
the cruise-only propeller is electrically connected to the first power source and is electrically disconnected from the second power source;
the hover-and-transition-only tiltrotor is electrically disconnected from the first power source and is electrically connected to the second power source;
during a cruise mode, the cruise-only propeller provides thrust by rotating using power from the first power source;
during a hovering mode and a transitional mode that occurs between the hovering mode and the cruise mode, the cruise-only propeller provides no thrust;
during the cruise mode, the hover-and-transition-only tiltrotor provides no thrust;
during the hovering mode and the transitional mode, the hover-and-transition-only tiltrotor provides thrust by rotating using power from the second power source; and
during a vertical landing in the hovering mode, the hover-and-transition-only tiltrotor switches power sources from the high energy battery to the high discharge rate battery, independent of a current draw.
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