Abstract: A continuous flow centrifuge bowl includes a rotatable outer body, and a top and bottom core that are rotatable with the outer body. The bottom core has a wall extending proximally from a bottom wall. The proximally extending wall is radially outward from at least a portion of the top core and, together with the top core, defines a primary separation region in which initial separation of the whole blood occurs. The bowl may also have a secondary separation region located between the top core and the outer body, and a rotary seal that couples an inlet port and two outlet ports to the outer body. The inlet port may be connected to an inlet tube that extends distally into a whole blood introduction region. Additionally, one of the outlet ports may be connected to an extraction tube that extends into a region below the bottom core.

Abstract: Methods and apparatus for automated calibration for a LIDAR system of a mobile robot are provided. The method comprises capturing a plurality of LIDAR measurements. The plurality of LIDAR measurements include a first set of LIDAR measurements as the mobile robot spins in a first direction at a first location, the first location being a first distance to a calibration target, and a second set of LIDAR measurements as the mobile robot spins in a second direction at a second location, the second location being a second distance to the calibration target, wherein the first direction and the second direction are different and the second distance is different than the first distance. The method further comprises processing the plurality of LIDAR measurements to determine calibration data, and generating alignment instructions for the LIDAR system based, at least in part, on the calibration data.

Abstract: Aspects of the present disclosure provide a wafer processing device for optimizing wafer shape. For example, the wafer processing device can include a first hot plate, a second hot plate and a controller. The first hot plate can be configured to heat a wafer. For example, the first hot plate can provide uniform heating across a surface of the first hot plate. The second hot plate has multiple heating zones with each heating zone independently controllable such that each heating zone can be set to a temperature value independent of other heating zones. The controller is configured to control the first hot plate to provide the uniform heating, receive a bow measurement from wafer curvature measurement of a wafer, and set the multiple heating zones of the second hot plate to their respective temperature values that correspond to the bow measurement.

Abstract: A radio frequency identification (RFID) system includes an array of antennas to distinguish line-of-sight (LOS) paths from non-line-of-sight (NLOS) paths. The distance between adjacent antennas in the array of antennas is less than half the wavelength of the radio frequency (RF) signal of the system. Each antenna in the antenna array is also digitally controlled to change relative phase difference among the antennas, thereby allowing digital steering of the array of antennas across angles of arrival (AOAs) between 0 and ?. The digital steering generates a plot of signal amplitudes as a function of AOAs. LOS paths are distinguished from NLOS paths based on the shapes (e.g., depth, gradient, etc.) of local extremes (e.g., maxima or minima) in the plot.

Abstract: Aspects of the present disclosure provide a wafer processing device for optimizing wafer shape. For example, the wafer processing device can include a first hot plate, a second hot plate and a controller. The first hot plate can be configured to heat a wafer. For example, the first hot plate can provide uniform heating across a surface of the first hot plate. The second hot plate has multiple heating zones with each heating zone independently controllable such that each heating zone can be set to a temperature value independent of other heating zones. The controller is configured to control the first hot plate to provide the uniform heating, receive a bow measurement from wafer curvature measurement of a wafer, and set the multiple heating zones of the second hot plate to their respective temperature values that correspond to the bow measurement.

Abstract: In certain embodiments, a method includes forming, by photolithography on a semiconductor wafer, first patterned features (PFs) including first photoresist structures (PRSs) having a first width and first recesses having a second width less than the first width and greater than a target width; forming, via anti-spacer patterning processing, second PFs including second PRSs having a third width less than the first width, first overcoat structures (OCSs) of the second width interspersed between second PRSs, and second recesses having a fourth width less than the target width; and forming, via acid diffusion processing, third PFs including third PRSs having a fifth width, second OCSs of the target width interspersed between third PRSs, and third recesses defined by third PRSs and second OCSs and having a sixth width greater than the fourth width, portions of first OCSs having been selectively removed using the acid diffusion processing to form second OCSs.

Abstract: A first intermediate representation of a first portion of a source code implementing an application and a second intermediate representation of a second portion of the source code is received by a processing device. The first intermediate representation and the second intermediate representation is merged, at run-time, into a merged intermediate representation, wherein the first intermediate representation includes a reference to a function in the second intermediate representation. An execution flow transfer instruction within the merged intermediate representation is identified based on a run-time value of a parameter of the application. The execution flow transfer instruction references the function. A set of executable instructions implementing the function is identified within the merged intermediate representation. The execution flow transfer instruction is replaced with a copy of the set of executable instructions implementing the function.

Abstract: Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially defined by the fuselage portion. In some embodiments, the aircraft assemblies disclosed herein comprise one or more first structural interfaces that permit positional adjustment between the wing unit and the fuselage portion so that one or more second structural interfaces may be finished only after such positional adjustment. In some embodiments, the aircraft assemblies disclosed herein comprise one or more structural interfaces that are disposed outside of the wing unit in order to eliminate or reduce the need for assembly personnel to access the interior of the wing unit to carry out the structural assembly of the wing unit to the fuselage portion.

Abstract: A rotor assembly for a peristaltic pump is provided. Each of a first pair of roller assemblies includes a first roller portion having a first diameter and a second roller portion having a second diameter. The first diameter is larger than the second diameter. Each of a second pair of roller assemblies includes a first roller portion having a first diameter and a second roller portion having a second diameter. The first diameter is smaller than the second diameter. The first and second pairs of roller assemblies are positionable around a circumference of a hub such that the first roller portion of the first pair of roller assemblies is aligned with the first roller portion of the second pair of roller assemblies and the second roller portion of the first pair of roller assemblies is aligned with the second roller portion of the second pair of roller assemblies.

Abstract: Methods and apparatus for implementing a safety system for a mobile robot are described. The method comprises receiving first sensor data from one or more sensors, the first sensor data being captured at a first time, identifying, based on the first sensor data, a first unobserved portion of a safety field in an environment of a mobile robot, assigning, to each of a plurality of contiguous regions within the first unobserved portion of the safety field, an occupancy state, updating, at a second time after the first time, the occupancy state of one or more of the plurality of contiguous regions, and determining one or more operating parameters for the mobile robot, the one or more operating parameters based, at least in part, on the occupancy state of at least some regions of the plurality of contiguous regions at the second time.

Abstract: Apparatuses, systems, and techniques to optimize processor performance. In at least one embodiment, a processor is to perform an application programming interface (API) to exclude one or more portions of program code from a program.

Abstract: In certain embodiments, a method includes depositing a photoresist layer over a semiconductor wafer to be patterned by photolithography, the photoresist layer having a first height, and exposing the photoresist layer to a pattern of actinic radiation to form exposed regions and non-exposed regions of the photoresist layer. The method further includes depositing an agent-containing layer over the photoresist layer and executing a post-exposure bake of the semiconductor wafer. The post-exposure bake modifies portions of the photoresist layer to form soluble portions of the photoresist layer for development. The soluble portions of the photoresist layer include the exposed regions and top portions of the non-exposed regions. The method further includes developing the photoresist layer to remove selectively the soluble portions, remaining portions of the non-exposed regions forming patterned structures of the semiconductor wafer and having a second height that is less than the first height.

Abstract: An assembly is provided for an aircraft. This aircraft assembly include an airframe with a horizontal axis. The aircraft assembly also includes a powerplant arranged with the airframe. The powerplant includes a gas turbine engine, an exhaust nozzle and a flowpath fluidly coupling the gas turbine engine to the exhaust nozzle. The exhaust nozzle includes a support structure and a plurality of nozzle flaps disposed on opposing sides of the flowpath. Each of the nozzle flaps is pivotally connected to the support structure. The exhaust nozzle is configured to exhaust combustion products received from the gas turbine engine along a first trajectory when the nozzle flaps are pivoted into a first arrangement. The first trajectory is angularly offset from the horizontal axis in a vertical upward direction.

Abstract: A kit includes a computing device configured to control motion of equipment for receiving one or more parcels in an environment of a mobile robot. The kit also includes a structure configured to couple to the equipment. The structure comprises an identifier configured to be sensed by a sensor of the mobile robot.

Abstract: A computing device receives location information for a mobile robot. The computing device also receives location information for an entity in an environment of the mobile robot. The computing device determines a distance between the mobile robot and the entity in the environment of the mobile robot. The computing device determines one or more operating parameters for the mobile robot. The one or more operating parameters are based on the determined distance.

Abstract: Assemblies and methods for facilitating the assembly of aircraft wings to a fuselage are disclosed. In some embodiments, a wing unit includes features that are configured to define one of more parts of a pressure vessel that is partially defined by the fuselage portion. In some embodiments, the aircraft assemblies disclosed herein comprise one or more first structural interfaces that permit positional adjustment between the wing unit and the fuselage portion so that one or more second structural interfaces may be finished only after such positional adjustment. In some embodiments, the aircraft assemblies disclosed herein comprise one or more structural interfaces that are disposed outside of the wing unit in order to eliminate or reduce the need for assembly personnel to access the interior of the wing unit to carry out the structural assembly of the wing unit to the fuselage portion.