Abstract: The present disclosure relates to a compound of Formula I wherein R is selected from the group consisting of —H, —F, —Cl, —Br, —I, —NO2, —CH3, and —C2H5; R1, R2, R3, R4 and R5 are independently selected from the group consisting of —H, —COOH, -, —CONH2, —COOCH3, —COOCH2CH3, —CN, —NO2, —OH, —CF3, —SO2NH2, —F, —Cl, —Br, —I, —OCH3, —CH3, and —COCH3, or a pharmaceutically acceptable salt thereof.

Abstract: An assembly is provided. The assembly includes a packaged semiconductor device and an outer enclosure enclosing the packaged semiconductor device. The assembly includes a packaged semiconductor device having a semiconductor chip and an outer enclosure enclosing the packaged semiconductor device. The packaged semiconductor device includes at least four opposing sides. The outer enclosure includes a magnetic material and further includes a lower section embedding the packaged semiconductor device, an upper section over the lower section, and a non-magnetic region arranged between the upper section and the lower section adjacent to the at least four opposing sides of the packaged semiconductor device.

Abstract: A method of calculating ionospheric scintillation includes calculating a motion-corrected perturbation of a GNSS radio signal received by a monitoring device deployed in an oceanic environment. The method includes calculating the ?? using the high rate phase of the GNSS signal adjusted by removing the change in distance between the monitoring device and the GNSS satellite. The calculating the ?? may further include passing the adjusted high rate phase through a high pass filter to remove a drift motion of the monitoring device. The method further includes calculating the S4 through calculating a tilt angle between the antenna of the monitoring device with the GNSS satellite and adjusting the antenna gain through known gain pattern of the antenna. The wave height of the oceanic environment may be calculated by detrending the antenna height to remove low frequency motion when a high rate position of the monitoring device is calculated.

Abstract: A method of operating a downhole system includes receiving trajectory data including a trajectory for steering a downhole tool toward a downhole target. The method includes identifying downhole tool data for the downhole tool. The method includes, based on the trajectory data and the downhole tool data, predicting one or more engineering metrics including one or more downhole tool metrics associated with an operation of the downhole tool in accordance with the trajectory and one or more completion metrics associated with a completion of the borehole at the downhole target. The method includes determining a coherency for the trajectory including determining whether the engineering metrics are within one or more predetermined thresholds. The method includes generating a report of at least some of the engineering metrics including a value of each engineering metric and an indication of whether the value is within the predetermined thresholds.

Abstract: Disclosed are compound, its stereoisomer, salt, hydrate, solvate, isotope or crystalline form thereof, represented by Formula (I), with X, R1, R2, R3, R4 and R5 as disclosed herein. Also, disclosed is a process for their preparation, compositions containing such compounds, methods of medical treatment or prophylaxis of a disease by such compounds and uses thereof. The compounds of Formula (I) are pyridoxal-5-phosphate (P5P) analogs, and can act as prodrugs.

Abstract: An assembly is provided. The assembly includes a packaged semiconductor device and an outer enclosure enclosing the packaged semiconductor device. The packaged semiconductor device includes at least four opposing sides. The outer enclosure includes a magnetic material and a non-magnetic region arranged adjacent to the at least four opposing sides of the packaged semiconductor device.

Abstract: Selective recovery of C2 to C4 hydrocarbons is achieved through the use of a converging-diverging nozzle, or de Laval nozzle. The vapor stream comprising C2 to C4 hydrocarbons is fed into an inlet of a de Laval nozzle having a throat. The vapor stream may have an initial temperature of between 0° C. and 100° C., and an initial pressure of between 200 psig and 500 psig. In the de Laval nozzle, the vapor stream expands after passing through the throat of the de Laval nozzle, producing a vapor stream having reduced temperature and pressure. Then, C2 to C4 hydrocarbons condense from the reduced-temperature vapor stream as liquid droplets, which may be recovered. Fractionation of C2 to C4 hydrocarbons by means of a de Laval nozzle is possible; the technique allows selective recovery of propane from a mixture of propane and ethane.

Abstract: A method of calculating ionospheric scintillation includes calculating a motion-corrected perturbation of a GNSS radio signal received by a monitoring device deployed in an oceanic environment. The method includes calculating the ?? using the high rate phase of the GNSS signal adjusted by removing the change in distance between the monitoring device and the GNSS satellite. The calculating the ?? may further include passing the adjusted high rate phase through a high pass filter to remove a drift motion of the monitoring device. The method further includes calculating the S4 through calculating a tilt angle between the antenna of the monitoring device with the GNSS satellite and adjusting the antenna gain through known gain pattern of the antenna. The wave height of the oceanic environment may be calculated by detrending the antenna height to remove low frequency motion when a high rate position of the monitoring device is calculated.

Abstract: A shield structure for a semiconductor chip comprises a chip mounting region on a base plate and a shell connected to the base plate. The shell is arranged over the base plate to provide a chamber having a volume, and the chip mounting region is arranged within the volume.

Abstract: A semiconductor device may include: a substrate; a protective region provided over the substrate; and a core structure enclosed by the protective region. The core structure may include a core material etchable by a chemical solution. The protective region may include a protective material resistant to etching by the chemical solution. The core structure may have a first side and a second side opposite to the first side, the first side being closer to the substrate than the second side. The core structure may be narrowest at the first side of the core structure.

Abstract: An example method of detecting an element using an autonomous vehicle includes the following operations: using a sensor on the autonomous vehicle to capture image data in a region of interest containing the element, where the image data represents components of the element; filtering the image data to produce filtered data having less of an amount of data than the image data; identifying the components of the element by analyzing the filtered data using a deterministic process; and detecting the element based on the components.

Abstract: An inductive device may be provided, including a first winding layer, a second winding layer arranged over the first winding layer and connected to the first winding layer to form a plurality of turns around a first axis, and a magnetic core arranged vertically between the first winding layer and the second winding layer. The magnetic core may include a portion entirely over the first winding layer and entirely under the second winding layer, where this portion may include a magnetic segment and a non-magnetic segment arranged laterally adjacent to each other along the first axis.

Abstract: An example method is performed by one or more processing devices and includes the following: identifying one or more features based on data obtained from a two-dimensional scan of a space, where the data includes predefined characteristics; identifying physical attributes of the one or more features; performing calculations based on the physical attributes for the one or more features, where the calculations produce one or more possible configurations for one or more candidate transport structures in the space; comparing the one or more possible configurations to one or more predefined configurations for one or more known transport structures; identifying which, if any, of the one or more candidate transport structures is most likely to be a known transport structure based on the comparing; and controlling an autonomous vehicle based on the identifying.

Abstract: An example method of detecting an element using an autonomous vehicle includes the following operations: using a sensor on the autonomous vehicle to capture image data in a region of interest containing the element, where the image data represents components of the element; filtering the image data to produce filtered data having less of an amount of data than the image data; identifying the components of the element by analyzing the filtered data using a deterministic process; and detecting the element based on the components.

Abstract: An assembly is provided. The assembly includes a packaged semiconductor device and an outer enclosure enclosing the packaged semiconductor device. The packaged semiconductor device includes at least four opposing sides. The outer enclosure includes a magnetic material and a non-magnetic region arranged adjacent to the at least four opposing sides of the packaged semiconductor device.

Abstract: A semiconductor device is provided. The semiconductor device comprises an inductor in a far back end of line layer and a capacitor adjacent to and electrically coupled with the inductor. The capacitor comprises a first electrode layer arranged over sidewalls and a bottom surface of a via in a first insulating layer A dielectric layer is provided over the first electrode layer. A second electrode layer is provided over the dielectric layer and a metal fill layer is provided over the second electrode layer. The metal fill layer has a top surface at least level with a top surface of the first insulating layer.

Abstract: An inductive device may be provided, including a substrate and an inductive structure arranged over the substrate. The inductive structure may include a bottom metal winding layer; a top metal winding layer arranged further away from the substrate than the bottom metal winding layer; a magnetic core layer arranged between the bottom metal winding layer and the top metal winding layer; a connector arranged to electrically connect the bottom metal winding layer and the top metal winding layer; and a top metal ring element arranged around the top metal winding layer, spaced apart from the top metal winding layer. The inductive device may further include a guard ring element arranged under the top metal ring element and around the magnetic core layer, spaced apart from the magnetic core layer; wherein the guard ring element may include a magnetic material.

Abstract: Selective recovery of C2 to C4 hydrocarbons is achieved through the use of a converging-diverging nozzle, or de Laval nozzle. The vapor stream comprising C2 to C4 hydrocarbons is fed into an inlet of a de Laval nozzle having a throat. The vapor stream may have an initial temperature of between 0° C. and 100° C., and an initial pressure of between 200 psig and 500 psig. In the de Laval nozzle, the vapor stream expands after passing through the throat of the de Laval nozzle, producing a vapor stream having reduced temperature and pressure. Then, C2 to C4 hydrocarbons condense from the reduced-temperature vapor stream as liquid droplets, which may be recovered. Fractionation of C2 to C4 hydrocarbons by means of a de Laval nozzle is possible; the technique allows selective recovery of propane from a mixture of propane and ethane.

Abstract: An inductive device may be provided, including a first winding layer, a second winding layer arranged over the first winding layer and connected to the first winding layer to form a plurality of turns around a first axis, and a magnetic core arranged vertically between the first winding layer and the second winding layer. The magnetic core may include a portion entirely over the first winding layer and entirely under the second winding layer, where this portion may include a magnetic segment and a non-magnetic segment arranged laterally adjacent to each other along the first axis.

Abstract: This system facilitates modification of application resources without modifying the source code of the application, while preventing modifications that may cause errors. After the source code and resources for an application are deployed, a user may provide a modified version of a resource, such as by changing a text string. The modified resource is compared to the existing version of the resource to determine if the modification will potentially cause an error when executing the application. If the modification adds or removes a parameter, changes a parameter name, changes a parameter type, or removes a resource, the change is prevented. Otherwise, the change is deployed without modifying the source code of the application. Parameters may be associated with hash codes or other types of identifiers to enable an application to locate a modified resource having a parameter that matches that of an original resource based on a matching identifier.