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: Apparatus and systems disclosed herein are designed to be used to study various forces acting on an athletic field or an athletic surface caused by the interaction between a shoe and the turf or athletic surface during a simulated impact. Various surfaces can be tested and analyzed, including assessing deceleration, acceleration and cutting traction potential on the surfaces. The disclosed apparatuses and systems allow for the testing of a wide variety of footwear, at any desired impact angle, and at various simulated forces. Methods, systems, and computer readable media for generating graphical representations associated with surface performance test information are also disclosed herein.

Abstract: An apparatus for a locking thermal conditioning hose for an electric aircraft, the apparatus comprising a thermal conditioning hose comprising a thermal medium flow path configured to contain a flow of a thermal medium, a thermal medium return path, the thermal medium return path configured to contain a flow of the thermal medium from an electric aircraft, and a mating component, wherein the mating component is configured to make a connection with an electric aircraft port, and a thermal latch, wherein the thermal latch is configured to couple the thermal conditioning hose to the electric aircraft.

Abstract: An Internet of Things (IoT) or vehicle dash cam may store both a high-resolution and low-resolution video stream on a device. The video streams are selectively accessible by remote devices. Because of the relatively smaller storage requirements of low-resolution video files, retaining of additional video data on the vehicle device (beyond what would be possible with only high-resolution video) is possible. The user may be provided an option to adjust the amount of low-resolution and high-resolution video to store on the device. A combined media file may be generated by a device to include time-synced high-resolution video, low-resolution video, and/or metadata for a particular time period.

Abstract: A system for thermal management ground service equipment and a method of use is disclosed. The system may include ground service equipment, wherein the ground service equipment may be configured to manage a temperature of a power source of an electric aircraft. The ground service equipment may include a coolant source, wherein the coolant source may include a reservoir containing a coolant. The ground service equipment may include a coolant heating system, wherein the coolant heating system may be configured to increase thermal energy of the coolant. The coolant heating system may include an electric resistance heating element. The system may include a controller communicatively connected to the ground service equipment, wherein the controller may be configured to receive an optimal temperature of the coolant and control the electric resistance heating element of the coolant heating system to increase the thermal energy of the coolant to the optimal temperature.

Abstract: Methods, apparatus, systems, and articles of manufacture are disclosed to rectify false set top box tuning data. Disclosed examples methods include identifying, by executing an instruction with a processor, in the return path data, first tuning data corresponding to a first group of set top boxes, the first group of set top boxes classified as associated with machine events, determining, by executing an instruction with a processor, a ratio between first tuning events in the return path data and second tuning events in the return path data, the first tuning events attributed to the first group of the set top boxes, the second tuning events attributed to a second group of the set top boxes classified at not associated with machine events, and in response to the ratio satisfying a threshold during a time interval, removing second tuning data associated with the time interval from the first tuning data.

Abstract: The present invention relates to a container for a consumable good having an inner coating layer comprising antioxidant, a process for preparing such a container, and the use of such container for the storage of a consumable good, and the use of antioxidant as an additive to coating layers of such containers.

Abstract: The invention relates to a container for a consumable good having an inner coating layer comprising an antioxidant, a process for preparing such a container, the use of such container for the storage of a consumable good, and the use of an antioxidant as an additive to a coating layer of such container.

Abstract: Methods of powering a radio that is mounted on a tower of a cellular base station are provided in which a direct current (“DC”) power signal is provided to the radio over a power cable and a voltage level of the output of the power supply is adjusted so as to provide a substantially constant voltage at a first end of the power cable that is remote from the power supply. Related cellular base stations and programmable power supplies are also provided.

Abstract: An apparatus for automated ground control of an electric vertical takeoff and landing aircraft includes a flight controller and a remote device. Remote device may transmit a location datum to a flight controller. Location datum may store a location of a charger, terminal, airport, or the like. Flight controller may authorize the location datum and direct aircraft using the information from the location datum.

Abstract: The disclosure relates to a sensitivity detection system that accurately and efficiently determines when information based on a user's browsing activity unintentionally reveals private or other sensitive information about the user. For example, the sensitivity detection system generates and utilizes machine learning models for detecting sensitivity to accurately detect when sensitive user information is being leaked from a collection of user information, such as a user profile. Additionally, upon determining that sensitive user information is being revealed, in many instances, the sensitivity detection system performs mitigation actions to stop and/or reduce sensitive user information from being undesirably revealed.

Abstract: A system for thermal management ground service equipment and a method of use is disclosed. The system may include ground service equipment, wherein the ground service equipment may be configured to manage a temperature of a power source of an electric aircraft. The ground service equipment may include a coolant source, wherein the coolant source may include a reservoir containing a coolant. The ground service equipment may include a coolant heating system, wherein the coolant heating system may be configured to increase thermal energy of the coolant. The coolant heating system may include an electric resistance heating element. The system may include a controller communicatively connected to the ground service equipment, wherein the controller may be configured to receive an optimal temperature of the coolant and control the electric resistance heating element of the coolant heating system to increase the thermal energy of the coolant to the optimal temperature.

Abstract: An apparatus for a locking thermal conditioning hose for an electric aircraft, the apparatus comprising a thermal conditioning hose comprising a thermal medium flow path configured to contain a flow of a thermal medium, a thermal medium return path, the thermal medium return path configured to contain a flow of the thermal medium from an electric aircraft, and a mating component, wherein the mating component is configured to make a connection with an electric aircraft port, and a thermal latch, wherein the thermal latch is configured to couple the thermal conditioning hose to the electric aircraft.

Abstract: Powder—based additive manufacturing processes for producing integral parts with multiple metallic materials are disclosed. The integral parts are printed as single pieces by joining different metallic materials together during printing. A combination of different powder-based additive manufacturing processes or the same process can be used to produce the integral part.

Abstract: A recording head comprises a write pole extending to an air-bearing surface. A near-field transducer is positioned proximate a first side of the write pole in a down-track direction. A heatsink structure is proximate the near-field transducer and positioned between the near-field transducer and the write pole. The heatsink structure extends beyond the near-field transducer in a cross-track direction and extends in a direction normal to the air-bearing surface.

Abstract: According to one aspect of the present disclosure, a system is provided which allows a network service provider to address providing service assurances to comply with each service level agreement (SLA) agreed to with customers. A translation system accesses one or more network service agreements and parses the one or more network service agreements into a processing format. The system then determines which network services are specified by the network service agreement, and determines service level agreements for each service. The translation system then generates one or more service level objectives for each service level agreement and one or more service level values for each service level objective. One or more metrics are then selected to be associated with each value to be measured to determine compliance with the service level agreement. The system then stores each of the service level agreements, objectives, values and metrics as objects.

Abstract: A showerhead (2) and a pulsation mechanism thereof are disclosed. The showerhead (2) with three sets of spaced-apart nozzles (22a, 22b, 22c) is configured to be cyclically activated in sequence, with each set of nozzles (22a, 22b, 22c) operative for approximately 0.25 seconds to 1 second, while the other two sets of nozzles (22a, 22b, 22c) are deactivated. The showerhead (2) includes a shutter (34) adapted to open a flow passage (36) within the showerhead (2) leading to one or more respective nozzles (22a, 22b, 22c) periodically to produce an intermittent pulsating flow.

Abstract: The present disclosure is directed to a blended wing body aircraft including a blended wing body, wherein the blended wing body is characterized by having no clear dividing line between wings and a main body along a leading edge of the aircraft; a cabin located within the main body and a transitional portion of the blended wing body; and a plurality of transmissive panels integrated into a ceiling of the cabin configured to transmit light from outside the blended wing body aircraft to inside the cabin.

Abstract: Aspects relate to a system for discharging a power source of an electric aircraft. System may be configured to transfer power from the electric aircraft via a charging connection. In one or more embodiments, a charging station in electric communication with the power source may discharge the power source. For example, a controller communicatively connected to the electric aircraft may be configured to receive a supply request from a user and subsequently, generate a control signal that initiates a transfer of electrical power from the power supply to discharge the power source so that power data associated with the discharge may be collected and transmitted to the controller or a remote device of the user.

Abstract: Disclosed herein are systems and methods for tracking an aircraft on a ramp. A system may receive a location datum and display the location datum to a user device. A location datum may include a machine vision datum.