Systems and methods for an electric vehicle charger

Patent metadata

Field	Value
Publication number	US-12512656-B2
Application number	US-202418761647-A
Country	US
Kind code	B2
Filing date	Jul 2, 2024
Priority date	May 23, 2022
Publication date	Dec 30, 2025
Grant date	Dec 30, 2025

Abstract

Embodiments of the disclosure provide an electric vehicle charger including a charger base housing an energy source, a charging cable coupled to the energy source, a charging connector for coupling the charging cable to an electric vehicle, and a cable storage device disposed within the charger base. The cable storage device includes: a reel rotatably disposed in the charger base. The charging cable is at least partially wrapped around the reel. A retraction mechanism is configured to rotate the reel to extend or retract the cable when activated. The retraction mechanism includes an electric motor operably coupled to the reel. A reel actuator is disposed on the charging connector and configured to activate the retraction mechanism. The reel actuator includes first and second user control elements for causing the electric motor to rotate in an extend or retract direction.

First claim

What is claimed is:

1 . An electric aircraft charger comprising:
a charger base housing an energy source; a charging cable coupled to the energy source; a charging connector for coupling the charging cable to an electric vehicle, wherein the charging connector includes a keying component shaped to prevent a pin of the charging connector from mating in an incorrect orientation; and a cable storage device disposed within the charger base, the cable storage device including: a reel rotatably disposed in the charger base, wherein the charging cable is at least partially wrapped around the reel; a retraction mechanism configured to rotate the reel to extend or retract the cable when activated, wherein the retraction mechanism is operably coupled to the reel; and a reel actuator disposed on the charging connector and configured to activate the retraction mechanism, the reel actuator including first and second user control elements for causing the reel to rotate in an extend or retract direction.

2 . The electric aircraft charger of claim 1 , further comprising a rotation toggle coupled to the reel and configured to adjust a rotation of the reel between the extend direction and the retract direction.

3 . The electric aircraft charger of claim 1 , wherein the charger base is mobile.

4 . The electric aircraft charger of claim 1 , wherein the charger base is proximal to a designated area for the electric vehicle within an operable range of the charging cable.

5 . The electric aircraft charger of claim 1 , further comprising a proximity detection pin within the charging connector, wherein the proximity detection pin is configured to detect electrical coupling of the charging connector to a port of the electric vehicle.

6 . The electric aircraft charger of claim 1 , wherein the charging connector includes a plurality of pins for electrically coupling the charging cable to the electric vehicle.

7 . An electric aircraft charger comprising:
a charger base housing an energy source; a charging cable coupled to the energy source; a charging connector coupling the charging cable to an electric aircraft, wherein the charging connector includes a keying component shaped to prevent a pin of the charging connector from mating in an incorrect orientation; and a cable storage device disposed within the charger base, the cable storage device including:
a reel rotatably disposed in the charger base, wherein the charging cable is at least partially wrapped around the reel;
a retraction mechanism configured to rotate the reel to extend and retract the cable when activated, wherein the retraction mechanism is operably coupled to the reel; and
a reel actuator disposed on the charging connector and configured to activate the retraction mechanism, the reel actuator including first and second user control elements for causing the reel to rotate in an extend or retract direction.

8 . The electric aircraft charger of claim 7 , further comprising a rotation toggle coupled to the reel and configured to adjust a rotation of the reel between the extend direction and the retract direction.

9 . The electric aircraft charger of claim 7 , wherein the charger base is mobile.

10 . The electric aircraft charger of claim 7 , wherein the charger base is proximal to a designated area for the electric aircraft within an operable range of the charging cable.

11 . The electric aircraft charger of claim 7 , further comprising a proximity detection pin within the charging connector, wherein the proximity detection pin is configured to detect electrical coupling of the charging connector to a port.

12 . The electric aircraft charger of claim 7 , wherein the charging connector includes a plurality of pins for electrically coupling the charging cable to the electric vehicle.

13 . An electric aircraft charger comprising:
a charger base housing an energy source; a charging cable coupled to the energy source; a charging connector for coupling the charging cable to an electric vehicle, wherein the charging connector includes a keying component shaped to prevent a pin of the charging connector from mating in an incorrect orientation; and a cable storage device disposed within the charger base, the cable storage device including: a reel rotatably disposed in the charger base wherein the charging cable is at least partially wrapped around the reel; a retraction mechanism configured to rotate the reel to extend and retract the charging cable when activated, wherein the retraction mechanism is operably coupled to the reel; and a reel actuator disposed on the charging connector and configured to activate the retraction mechanism, the reel actuator including first and second user control elements for causing the reel to rotate in an extend or retract direction; and a rotation toggle coupled to the reel and configured to adjust a rotation of the reel between the extend direction and the retract direction.

14 . The electric aircraft charger of claim 13 , wherein the charger base is mobile.

15 . The electric aircraft charger of claim 13 , wherein the charging connector includes a plurality of pins for electrically coupling the charging cable to the electric vehicle.

16 . The electric aircraft charger of claim 13 , wherein the rotation toggle is on one of the charging connector or an exterior surface of the charger base.

17 . The electric aircraft charger of claim 13 , further comprising a proximity detection pin within the charging connector, wherein the proximity detection pin is configured to detect electrical coupling of the charging connector to a port of the electric vehicle.

18 . The electric aircraft charger of claim 13 , wherein the charger base is proximal to a designated area for the electric vehicle within an operable range of the charging cable.

Assignees

• Beta Air Llc

Inventors

• Palombini John Charles
• Carapetyan Skye
• Donnelly Richard
• Pill Jake
• Hall Edward
• Hanson Cole William
• Whitehill James

Classifications

• B64F1/35

  for supplying electrical power to stationary aircraft · CPC title

• B60L2200/10

  Air crafts · CPC title

• B65H75/4486

  Electric motors · CPC title

• B60L53/18

  Cables specially adapted for charging electric vehicles · CPC title

• B60L53/53

  Batteries · CPC title