Charging station for self-balancing multicopter
A vertical landing is performed by an electric vertical take-off and landing (eVTOL) vehicle above a charger where the eVTOL vehicle includes a rotor that is configured to rotate during an occupant change state to keep the eVTOL vehicle stationary during the occupant change state. A vertically-oriented male charging port that is part of the eVTOL vehicle and a female charging port that is part of the charger are detachably coupled and a battery in the eVTOL vehicle is charged using the charger while the vertically-oriented male charging port and the female charging port are detachably coupled.
1. An electric vertical take-off and landing (eVTOL) vehicle, comprising:
a controller that is configured to perform a vertical landing by the eVTOL vehicle above a charger;
a rotor that is configured to rotate during occupant boarding to keep the eVTOL vehicle stationary during occupant boarding; and
a vertically-oriented male charging port that is:
provided on an underside of the eVTOL vehicle, and
configured to charge a battery in the eVTOL vehicle including by detachably coupling the vertically-oriented male charging port that is part of the eVTOL vehicle and a female charging port that is part of the charger.
2. The eVTOL vehicle recited in claim 1 , wherein the vertically-oriented male charging port is retractable and detachably coupling the vertically-oriented male charging port and the female charging port includes extending the vertically-oriented male charging port.
3. The eVTOL vehicle recited in claim 1 , wherein:
the eVTOL vehicle further includes a seatback compartment which includes the battery; and
the vertically-oriented male charging port is retractable and detachably coupling the vertically-oriented male charging port and the female charging port includes extending the vertically-oriented male charging port outward from the seatback compartment.
4. The eVTOL vehicle recited in claim 1 , wherein:
the eVTOL vehicle is an ultralight, open air vehicle that further includes a seatback compartment which includes the battery; and
the vertically-oriented male charging port is retractable and detachably coupling the vertically-oriented male charging port and the female charging port includes extending the vertically-oriented male charging port outward from the seatback compartment.
5. The eVTOL vehicle recited in claim 1 , wherein:
the charger is located in a secured area that includes a plurality of chargers; and
the controller is further configured to communicate with a secured area controller to receive an assignment of the charger from the plurality of chargers in the secured area for the eVTOL vehicle to perform the vertical landing above.
6. A method, comprising:
performing a vertical landing by an electric vertical take-off and landing (eVTOL) vehicle above a charger, wherein the eVTOL vehicle includes a rotor that is configured to rotate during an occupant change state to keep the eVTOL vehicle stationary during the occupant change state;
detachably coupling a vertically-oriented male charging port that is part of the eVTOL vehicle and a female charging port that is part of the charger, wherein the vertically-oriented male charging port is provided on an underside of the eVTOL vehicle; and
charging a battery in the eVTOL vehicle using the charger while the vertically-oriented male charging port and the female charging port are detachably coupled.
7. The method recited in claim 6 , wherein the vertically-oriented male charging port is retractable and detachably coupling the vertically-oriented male charging port and the female charging port includes extending the vertically-oriented male charging port.
8. The method recited in claim 6 , wherein:
the eVTOL vehicle further includes a seatback compartment which includes the battery; and
the vertically-oriented male charging port is retractable and detachably coupling the vertically-oriented male charging port and the female charging port includes extending the vertically-oriented male charging port outward from the seatback compartment.
9. The method recited in claim 6 , wherein:
the eVTOL vehicle is an ultralight, open air vehicle that further includes a seatback compartment which includes the battery; and
the vertically-oriented male charging port is retractable and detachably coupling the vertically-oriented male charging port and the female charging port includes extending the vertically-oriented male charging port outward from the seatback compartment.
10. The method recited in claim 6 , wherein:
the charger is located in a secured area that includes a plurality of chargers; and
the method further includes communicating with a secured area controller to receive an assignment of the charger from the plurality of chargers in the secured area for the eVTOL vehicle to perform the vertical landing above.
11. A computer program product, the computer program product being embodied in non-transitory computer readable storage medium and comprising computer instructions for:
performing a vertical landing by an electric vertical take-off and landing (eVTOL) vehicle above a charger, wherein the eVTOL vehicle includes a rotor that is configured to rotate during an occupant change state to keep the eVTOL vehicle stationary during the occupant change state;
detachably coupling a vertically-oriented male charging port that is part of the eVTOL vehicle and a female charging port that is part of the charger, wherein the vertically-oriented male charging port is provided on an underside of the eVTOL vehicle; and
charging a battery in the eVTOL vehicle using the charger while the vertically-oriented male charging port and the female charging port are detachably coupled.
12. The computer program product recited in claim 11 , wherein the vertically-oriented male charging port is retractable and the computer instructions for detachably coupling the vertically-oriented male charging port and the female charging port include computer instructions for extending the vertically-oriented male charging port.
13. The computer program product recited in claim 11 , wherein:
the eVTOL vehicle further includes a seatback compartment which includes the battery; and
the vertically-oriented male charging port is retractable and the computer instructions for detachably coupling the vertically-oriented male charging port and the female charging port include computer instructions for extending the vertically-oriented male charging port outward from the seatback compartment.
14. The computer program product recited in claim 11 , wherein:
the eVTOL vehicle is an ultralight, open air vehicle that further includes a seatback compartment which includes the battery; and
the vertically-oriented male charging port is retractable and the computer instructions for detachably coupling the vertically-oriented male charging port and the female charging port include computer instructions for extending the vertically-oriented male charging port outward from the seatback compartment.
15. The computer program product recited in claim 11 , wherein:
the charger is located in a secured area that includes a plurality of chargers;
the computer program product further includes computer instructions for communicating with a secured area controller to receive an assignment of the charger from the plurality of chargers in the secured area for the eVTOL vehicle to perform the vertical landing above.
16. The eVTOL vehicle recited in claim 1 , further comprising the battery.
17. The eVTOL vehicle recited in claim 1 , further comprising a vertical spar, wherein the rotor is mounted on the vertical spar to provide separation between the rotor and an occupant of the eVTOL vehicle.
18. The eVTOL vehicle recited in claim 17 , wherein the vertically-oriented male charging port is provided on a bottom portion of the vertical spar.