Abstract: A document analysis system (100) for use by legal or business users is described. The system (100) includes a number of user devices 102 that communicate with a processing platform (104) to upload documents and receive reports concerning the documents. The illustrated platform (104) includes a processor (112), a document database (114), a preprocessing module (115), a machine learning module (116), a repository for analytics (118), and a report generator (120). A user can upload contracts or other documents to the platform (104) and receive scoring and ratings information for the contract.

Abstract: Disclosed herein are compounds and ligands, and compositions formed therewith, that modulate insulin secretion and suppress appetite by activating ectopic olfactory receptors. Also disclosed herein are methods for using the compositions to treat endocrine diseases, such as type-2 diabetes, and disorders, such as abnormal insulin secretion.

Abstract: An optical fiber cable that includes subunits is provided. The cable has an outer jacket having a thickness of at least 2.0 millimeters and that is made from a fire retardant polymer material having a PHRR value of 222 kw/m2 when tested in a cone calorimeter measured according to ASTM E1354 with a heat flux of 50 kW/m2. The cable meets the requirement of UL 1666 burn test for riser cables and the requirements of EN 50399 burn test for CPR class Cca cables.

Abstract: A thermal energy storage and power generation system includes a thermal energy storage device including a container, a heating element in the container, a pair of fins in the container and arranged on opposite sides of the heating element, a thermal storage material in the container, and a tube in the container and extending around the thermal storage material. The system also includes a generator in communication with the thermal energy storage device for converting thermal energy into electrical energy as well as subsystems for regulating and controlling the system.

Abstract: A ground service system for an electric aircraft is disclosed. The system includes a charging module including a charging cable electrically connected to an energy source and configured to charge a battery of the electric aircraft. The system also includes a cooling module including a cooling channel configured to fluidly couple the electric aircraft to a coolant source. The cooling module is configured to transmit a coolant from the coolant source and through the cooling channel to the electric aircraft to regulate a temperature of the battery of the electric aircraft. A controller of the cooling module is in communication with a battery management controller of the electric aircraft through a controller of the charging module.

Abstract: A roll end air fitting adapter is couplable to an end of a cylindrical roll. The adapter includes an inner ring and outer ring defining a central opening concentric with a roll axis, an annular air channel extending about the roll axis, and a plurality of air passages leading from the air channel through the inner ring and/or the outer ring to peripheral outlet openings in an outer circumferential surface(s) of the inner ring and/or the outer ring. A compliant sleeve is disposed along the roll axis with the peripheral outlet openings between the end of the compliant sleeve and the outer ring so that the compliant sleeve overlaps the peripheral outlet openings. Supplying air to the adapter ring by the air source to force air through the air channel and the peripheral outlet openings facilitates sliding the compliant sleeve onto the cylindrical roll.

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.

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: 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: 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: 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: This invention is directed to a polymeric powder preferably a medical grade polymeric powder, for use in Selective Laser Sintering (SLS) for application fields including but not limited to medical, food, and pharmaceutical. The, preferably medical grade, polymer is biodegradable and can be used to manufacture objects such as medical implants and tissue scaffolds. The powder is biocompatible and biodegradable and can include a flow additive. The flow additive can consist of an osteoconductive flow aid suited for medical applications, a water-soluble salt flow aid that does dissolve during device degradation, or a combination of both. The water-soluble salt flow aid is used for applications where no leftover signs of implantation are observed within tissue after device degradation.

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.