Abstract: In an aspect a system for electric charger communication is presented. A system includes a first networking component and sensor of a first electric charger. The system includes at least a processor communicatively connected to a first networking component and the sensor. The system includes memory communicatively connected to at least a processor, wherein the memory contains instructions configuring at least a processor to receive the at least a charger metric from the sensor and transmit the at least a charger metric to the network using the first communicative connection, wherein the at least a charger metric comprises a charger status.

Abstract: A system for an electric vehicle charger with a reel button for an electric vehicle is illustrated. The system comprises a charging cable, a charger base connected to the charging cable, a cable storage device, the cable storage device including a retraction mechanism configured to pay out and retract the cable when activated and at least a reel button configured to activate the retraction mechanism.

Abstract: A ground service system for an electric aircraft is disclosed. The system includes a charging module configured to charge a battery of an electric aircraft. The charging module includes a charging cable electrically connected to an energy source. The system includes a cooling module configured to regulate a temperature of the battery. The cooling module includes a cooling cable configured to carry a coolant. The system also includes a cabin soak module configured to provide a cabin soak coolant to a cabin of the electric aircraft. The cabin soak module includes a cabin soak cable configured to carry a fluid.

Abstract: An apparatus and method for a recharging station including a landing pad, a rechargeable component coupled to the landing pad, and a power delivery unit configured to deliver power from a power supply unit or power storage unit to the recharging component. Rechargeable component includes a plurality of charging units placed at predetermined spacings from one another. The plurality of charging units allows for the electric aircraft to land in any orientation.

Abstract: Electric aircraft charging system including charging cable configured to carry electricity and energy source, wherein the energy source is electrically connected to the charging cable. The system also including a cable reel module, the cable reel module including a reel, wherein the reel is rotatably mounted to the cable reel module, wherein the reel is configured to rotate in a forward direction and a reverse direction, and the charging cable, in a stowed configuration, is wound around the reel. The cable reel module further including a rotation mechanism configured to rotate the reel in reverse, and a cable reel module door having a closed position and an open position, wherein the closed position prevents access to the reel and the open position allows access to the reel. The system additionally including a controller communicatively connected to the rotation mechanism and configured to send a retraction signal to the rotation mechanism.

Abstract: Motorcycle riders, being more vulnerable than drivers of four-wheeled vehicles, can especially benefit from advance warnings of hazards. Hazards are detected in the predicted path of the motorcycle or are predicted to be in the path within the next few seconds of the motorcycle's travel. The outputs from the sensors that detect the hazards are corrected for the lean of the motorcycle as it corners. The predicted path or ego lane of the motorcycle is also adjusted depending on the lean of the motorcycle.

Abstract: An apparatus and method for a recharging station including a landing pad, a rechargeable component coupled to the landing pad, and a power delivery unit configured to deliver power from a power supply unit or power storage unit to the recharging component. Rechargeable component includes a plurality of charging units placed at predetermined spacings from one another. The plurality of charging units allows for the electric aircraft to land in any orientation.

Abstract: A ground service system for an electric aircraft is disclosed. The system includes a charging module configured to charge a battery of an electric aircraft. The charging module includes a charging cable electrically connected to an energy source. The system includes a cooling module configured to regulate a temperature of the battery. The cooling module includes a cooling cable configured to carry a coolant. The system also includes a cabin soak module configured to provide a cabin soak coolant to a cabin of the electric aircraft. The cabin soak module includes a cabin soak cable configured to carry a fluid.

Abstract: Electric aircraft charging system including charging cable configured to carry electricity and energy source, wherein the energy source is electrically connected to the charging cable. The system also including a cable reel module, the cable reel module including a reel, wherein the reel is rotatably mounted to the cable reel module, wherein the reel is configured to rotate in a forward direction and a reverse direction, and the charging cable, in a stowed configuration, is wound around the reel. The cable reel module further including a rotation mechanism configured to rotate the reel in reverse, and a cable reel module door having a closed position and an open position, wherein the closed position prevents access to the reel and the open position allows access to the reel. The system additionally including a controller communicatively connected to the rotation mechanism and configured to send a retraction signal to the rotation mechanism.

Abstract: A system for charging an electric aircraft including a horizontal cable arrangement, including a charger base including an energy source and a charging cable electrically connected to the energy source. The system further including a horizontal cable including at least a length of the charging cable and having a first cable arrangement position, wherein the horizontal cable arrangement is located at a first elevation, and a second cable arrangement position, wherein the horizontal cable arrangement is located at a second elevation. The second elevation is greater than the first elevation. The system further including a lift in contact with the horizontal cable arrangement. The lift having a first lift position and a second lift position. In the first lift position, the horizontal cable arrangement is in the first cable arrangement position, and in the second lift position, the horizontal cable arrangement is in the second cable arrangement position.

Abstract: A system for charging an electric aircraft including a vertical cable arrangement, the system including a charger. The charger including an energy source, a charging cable electrically connected to the energy source, and a vertical cable arrangement. The vertical cable arrangement has a first cable arrangement position wherein the vertical cable arrangement is located at a first elevation, and has a second cable arrangement position, wherein the vertical cable arrangement is located at a second elevation, wherein the second elevation is greater than the first elevation. The charger also includes a lift connected to the vertical cable arrangement. The lift has a first lift position and a second lift position. When the lift is in the first lift position, the vertical cable arrangement is in the first cable arrangement position. When the lift is in the second lift position, the vertical cable arrangement is in the second cable arrangement position.

Abstract: A quick connect terminal assembly for attaching a conductor to an electrical circuit includes a terminal which can be attached to an electrical circuit. A retainer engages the terminal which defines a conductor space between the retainer and the terminal. The conductor space insertably receives an end of a conductor. The retainer is biased toward the terminal to compress the conductor between the terminal and the retainer. Each of the retainer and the terminal is comprised of an electrically conductive material to facilitate electrical communication between the conductor and the electrical circuit. A sheath is positioned around the terminal and the retainer to inhibit electrical communication between the conductor and external objects.

Abstract: A separator vessel has inlet, fluid outlet, and sand outlet ports. Each of the fluid and sand outlet ports are spaced below the inlet port. The separator has an enclosure between the inlet and fluid outlet ports. The enclosure redirects the fluid stream and defines an inner cavity above a lower edge of the enclosure, the lower edge defining a liquid flow area. The separator has one or more vanes extending along an outer surface of the enclosure which redirect the fluid stream along a curved flow path as the fluid stream flows toward the lower edge, and a plurality of apertures adjacent to the vanes, the apertures permitting fluid flow into the inner cavity of the enclosure. The fluid outlet port is disposed within the inner cavity above the lower edge of the enclosure and below one or more apertures.

Abstract: A separator vessel has inlet, fluid outlet, and sand outlet ports. Each of the fluid and sand outlet ports are spaced below the inlet port. The separator has an enclosure between the inlet and fluid outlet ports. The enclosure redirects the fluid stream and defines an inner cavity above a lower edge of the enclosure, the lower edge defining a liquid flow area. The separator has one or more vanes extending along an outer surface of the enclosure which redirect the fluid stream along a curved flow path as the fluid stream flows toward the lower edge, and a plurality of apertures adjacent to the vanes, the apertures permitting fluid flow into the inner cavity of the enclosure. The fluid outlet port is disposed within the inner cavity above the lower edge of the enclosure and below one or more apertures.

Abstract: Devices for detecting electrical activity in electrically active biological tissues and methods for using the devices are provided. The devices include an electrode array that is configured for implantation on electrically active biological tissue. The electrode array comprises a plurality of electrode sites comprising one or more layers of transparent, electrically conductive graphene disposed on a transparent substrate.

Abstract: Articles of clothing, such as gloves having a substantially seamless inner liner and methods of manufacturing the same are disclosed herein. In one embodiment, a process for manufacturing a glove comprises stretching an outer layer inside-out over a glove form, such that an interior surface of the outer layer faces outward. A liner having a first side and a second side opposite the first side is cut from a fabric, such as fleece. An adhesive is deposited in an adhesive pattern onto the first side of the liner. The adhesive fuses to the interior surface of the outer layer in a heat/pressure procedure, thereby affixing the first side of the liner to the interior surface of the outer layer to form the glove. The glove is removed from the glove form and inverted to a right-side-out configuration, thereby compressing the outer layer and the liner.

Abstract: A disposable absorbent article is presenting having multiple components and including an inspection region subject to inspection using infrared radiation, wherein the inspection region includes a junction of two components; and a printed graphic in the inspection region, wherein the ink used to print the graphic includes no carbon black colorant such that the printed graphic is substantially transparent to infrared radiation. In addition, a disposable absorbent article having multiple components includes a printed graphic in an inspection region subject to inspection using infrared radiation, the printed graphic including black ink having no carbon black colorant such that the printed graphic is substantially transparent to infrared radiation.

Abstract: Waterproof touchscreen gloves and associated clothing articles and methods of manufacturing the same are disclosed herein. In one embodiment, a waterproof touchscreen glove comprises an electrically conductive inner layer defining an interior region that receives a user hand, an electrically conductive outer layer, and a substantially continuous and unpenetrated waterproof layer between the inner layer and the outer layer.

Abstract: Devices for detecting electrical activity in electrically active biological tissues and methods for using the devices are provided. The devices include an electrode array that is configured for implantation on electrically active biological tissue. The electrode array comprises a plurality of electrode sites comprising one or more layers of transparent, electrically conductive graphene disposed on a transparent substrate.

Abstract: Articles of clothing, such as gloves having a substantially seamless inner liner and methods of manufacturing the same are disclosed herein. In one embodiment, a process for manufacturing a glove comprises stretching an outer layer inside-out over a glove form, such that an interior surface of the outer layer faces outward. A liner having a first side and a second side opposite the first side is cut from a fabric, such as fleece. An adhesive is deposited in an adhesive pattern onto the first side of the liner. The adhesive fuses to the interior surface of the outer layer in a heat/pressure procedure, thereby affixing the first side of the liner to the interior surface of the outer layer to form the glove. The glove is removed from the glove form and inverted to a right-side-out configuration, thereby compressing the outer layer and the liner.