Abstract: A system for visualization and management of participants in studies having a graphical user interface (GUI), a database (DB) storing studies data, visit schedules, travel policies, sites data, and participants data having a first participant in a first study. The GUI has controls including system control, data controls (being one or more of a travel policy control, visit schedule control, and participant control), navigation control associated with the study, and selection control associated with the participant. The GUI responsive to using the controls can a) switch GUI views; b) receive and display participants data; c) receive and display visit schedule and travel policy associated with the first participant and with the first study; d) receive input data from the input device and cause the DB to update the studies data, participants data, travel policies, and visit schedules with the input data. DB may store a second participant.

Abstract: Systems for visualization and management of a clinical study have a processor, an input device, a database storing data related to the clinical study, and a visit schedule interface. The data have a study visit schedule. The study visit schedule has nodes and a track having a step sequence. Each node has a node position and node attributes. The node position has a node track identifying the track and a node step. The data may also have a visit travel policy and the node attributes may have a visit policy label associated with the visit travel policy.

Abstract: A capillary tube holder is provided for holding a capillary tube. The capillary tube holder includes a holder insert and a holder base. The holder insert includes a capillary groove configured for receiving the capillary tube. The holder base is configured for slidably receiving and retaining the holder insert therein.

Abstract: An aircraft propulsion system is provided that includes a turbine engine and an intercooler (IC). The turbine engine includes a source of non-hydrocarbon fuel, and a low pressure compressor having an LPC air inlet and outlet, and a high pressure compressor having an HPC air inlet and outlet. The intercooler has an IC air inlet, an IC air outlet, a U-shaped air passage, and crossflow tubes. The IC air inlet is in fluid communication with the LPC air outlet. The IC air outlet is in fluid communication with the HPC air inlet. The U-shaped air passage is in fluid communication with the IC air inlet and outlet. The crossflow tubes extend through the U-shaped air passage. The crossflow tubes are in fluid communication with the source of non-hydrocarbon fuel, and are configured to contain a flow of the non-hydrocarbon fuel therethrough.

Abstract: A method for automated online proctoring, in accordance with one embodiment, includes using an AI system to consider monitored aspects of activities of a student taking a test to calculate a trust score indicative of academic integrity, the aspects including at least user interaction with one or more input devices, and eye movements of the student. The AI system is used to provide guidance to the student during the test for improving a submission input by the student during the test. An automated online proctoring system, in accordance with one embodiment, includes a facial recognition module; a lockdown test monitor module; and an AI system configured to consider a plurality of monitored aspects of activities of the student to calculate a trust score that characterizes an authenticity and originality of a submission by the student during the test, and to provide guidance to the student during the test.

Abstract: In accordance with at least one aspect of this disclosure, there is provided a system for an aircraft engine. In embodiments, the system includes an accessory box and a fuel accessory located in an interior space within the accessory box, where a vent is defined through a wall of the accessory box. In embodiments, the vent includes a plurality of holes or slots in an outer wall of the accessory box for passage of gaseous fuel from the interior space. In embodiments, the vent is configured for passive ventilation of the interior space.

Abstract: A joist pocket assembly and a method for manufacturing a joist pocket assembly is described herein. In some embodiments, the joist pocket assembly can include a frame configured to be mounted within a cut-out in a wall. In some embodiments, the joist pocket assembly can include a base of the frame, where the base can be configured to receive a structural member of a joist. In some embodiments, the joist pocket assembly can include a flange extending from a perimeter of the frame, where the flange can cover a gap between the frame and the wall. In some embodiments, the joist pocket assembly can include a first stud coupled to the base of the frame, where the first stud can secure the frame to the wall. In some embodiments, the joist pocket assembly can be placed in a concrete tilt wall or concrete precast wall.

Abstract: Systems and methods may use models to generate predictions of specific access rights for users. Further, systems and methods may generate the predictions in an environment in which the availability of the specific access rights change frequently. The access rights, predicted using embodiments described herein, may be both available and associated with user affinities. An interface associated with the primary load management system may be configured to display the predicted access rights for a user operating a user device.

Abstract: An electronic indicator on a see-through optical scope indicates whether an optical system is canted. The visual indicator may include one or more LEDs coupled to a microprocessor that is also coupled to a solid-state electronic inclinometer incorporated into the internal structure of the optical system. The microprocessor is configured to selectively illuminate the visual indicator based on the output of the inclinometer, thereby indicating how the reticle is canted, if at all.

Abstract: The present disclosure relates to the field of tissue dissection. Specifically, the present disclosure relates to medical devices which lift and retract tissue during a dissection procedure to improve visualization of the target tissue and mitigate obstruction of dissection tools. In particular, the present disclosure relates to a tissue retraction device which moves from a constrained to relaxed configuration to immobilize and retract the dissected portion of target tissue during a dissection procedure.

Abstract: A method for determining a trust indicator is provided. The method may include interpreting, via an Internet of Things Universal Identifier (IoT UID) processing circuit, an IoT UID corresponding to a device and identifying, via a record management circuit and based at least in part on the IoT UID, a record in a database corresponding to the device. The method may further include determining, via a trust analysis circuit and based at least in part on the record, a risk indicator of the device and transmitting, via an indicator provisioning circuit, the risk indicator.

Abstract: The present disclosure is directed to human monoclonal IgE antibodies, and IgG antibodies engineered therefrom. Such engineered antibodies can be used to blunt pathologic IgE responses in subjects, such as in the treatment or prevention of allergies.

Abstract: An aircraft propulsion system is provided that includes a turbine engine and an exhaust gas heat exchanger. The exhaust gas heat exchanger includes a central conduit, an outer radial plenum, fluid conduits, and inter-conduit passages. The fluid conduits are disposed in a nested arrangement. Each fluid conduit has inner and outer radial walls that extend axially between the forward and aft ends. The inner and outer radial walls are radially separated to form an internal fluid passage. Each fluid conduit is radially spaced apart from adjacent fluid conduits to define an axially extending exhaust gas passages. The inter-conduit passages include at least one inter-conduit passage that provides fluid communication between the central conduit and a first fluid conduit, and at least one inter-conduit passage that provides fluid communication between first and second fluid conduits. A serpentine fluid flow path extends through the fluid conduits and the inter-conduit passages.

Abstract: Mounting bracket assemblies including first, second and third bracket members. The first bracket member includes first and second mounting surface portions. The first mounting surface portion engaging a suspension component. The second mounting surface portion defining a receiving zone for receiving a vehicle structure and is disposed along a first side of a first central plane of the receiving zone. A second bracket member includes first and second contact surface portions. The second bracket member is disposed along a second side of the first central plane and along a first side of a second central plane of the receiving zone. A third bracket member includes third and fourth contact surface portions. The third bracket member is disposed along the second side of the first central plane and along a second side of the second central plane. Suspension systems, kits and methods are also included.

Abstract: An aircraft propulsion system is provided that includes a turbine engine and an intercooler (IC). The turbine engine includes a source of non-hydrocarbon fuel, and a low pressure compressor having an LPC air inlet and outlet, and a high pressure compressor having an HPC air inlet and outlet. The intercooler has an IC air inlet, an IC air outlet, a U-shaped air passage, and crossflow tubes. The IC air inlet is in fluid communication with the LPC air outlet. The IC air outlet is in fluid communication with the HPC air inlet. The U-shaped air passage is in fluid communication with the IC air inlet and outlet. The crossflow tubes extend through the U-shaped air passage. The crossflow tubes are in fluid communication with the source of non-hydrocarbon fuel, and are configured to contain a flow of the non-hydrocarbon fuel therethrough.

Abstract: An aircraft propulsion system and method is provided. The system includes compressor, combustor, and turbine sections, a fuel source, a heat exchanger, a compressor bleed air passage, and a cooling air passage. The fuel source is configured to contain a non-hydrocarbon fuel. The heat exchanger has separate air and fuel passages. The air passage permits passage of the compressed air therethrough. The fuel passage is configured to permit a passage of the non-hydrocarbon fuel therethrough. The compressor bleed air passage is configured to receive compressed air bleed off a core flow path upstream of the combustor section. The compressor bleed air passage is in fluid communication with the air passage air inlet. The cooling air passage is configured to receive compressed air exiting the air passage air outlet and configured to direct the compressed bleed air to the vane stage or rotor stage of the turbine section, or both.

Abstract: An engine system is provided that includes an open propulsor rotor, an engine core assembly, a bypass flowpath and a condenser. The engine core assembly is configured to drive rotation of the open propulsor rotor. The engine core assembly includes a core flowpath, a compressor section, a combustor section and a turbine section. The core flowpath extends through the compressor section, the combustor section and the turbine section from an inlet into the core flowpath to an exhaust from the core flowpath. The bypass flowpath bypasses the engine core assembly. The condenser is configured to exchange heat energy between combustion products flowing within the core flowpath downstream of the combustor section and bypass air flowing within the bypass flowpath.

Abstract: An engine system includes an engine core assembly, a fuel system and a cooling circuit. The engine core assembly includes a core flowpath, a compressor section, a combustor section and a turbine section. The combustor section includes a combustor adjacent a plenum. The fuel system includes a fuel flowpath, a fuel reservoir, a fuel-cooling air heat exchanger and a fuel injector. The fuel flowpath is configured to direct hydrogen fuel, received from the fuel reservoir, through the fuel-cooling air heat exchanger to the fuel injector. The fuel injector is configured to introduce the hydrogen fuel into the combustor. The cooling circuit is configured to direct cooling air, bled from the plenum, through the fuel-cooling air heat exchanger to the turbine section. The fuel-cooling air heat exchanger is configured to exchange heat energy between the hydrogen fuel flowing within the fuel flowpath and the cooling air flowing within the cooling circuit.

Abstract: An oven vent heat diverter device is disclosed which is a heat diversion barrier placed under the control panel of an oven or other appliance and redirects the heat to the exhaust fan. The oven vent heat diverter device comprises a body component consisting of several hinged panels attached to one another. In use, the hinged panels are secured together in a square configuration and positioned over the cooking surface of the free-standing range vent area, and under a control panel of an over-the-range (OTR) microwave or other suitable oven appliance. Further, the device can be folded up substantially flat for easy and convenient storage.

Abstract: Provided are a computer product, system, and method for dynamic assignment of device queues to virtual functions to provide to virtual machines. Queues are assigned to a virtual function to access the physical functions of the device. The virtual function is provided to a virtual machine to use to access the physical functions of the device. A determination is made of a utilization of the queues assigned to the virtual function accessed by the virtual machine. A number of the queues assigned to the virtual functions for requests submitted by the virtual machine is changed in response to the determined utilization.