Abstract: An assembly and method for delivery of an analyte sensor including a reusable applicator having a proximal portion and a distal portion are disclosed. The reusable applicator can include a housing, a sensor carrier configured to releasably receive the first analyte sensor, a sharp carrier configured to releasably receive a sharp module, and an actuator movable relative to the housing.

Abstract: An additive manufacturing powdered composite material includes metal particles coated with a coating of ceramic particles. The metal particles may include a ternary NiCoCr alloy, with select additions of minor amounts of other elements. The ceramic particles may include yttrium oxide or other oxides. The composite material is suitable for additive manufacturing (AM) into a component for high temperature (>1000° C.) applications. The AM component includes a metal matrix formed from the alloy, with the ceramic particles dispersed in the matrix.

Abstract: A collapsible ladder with steps that remained stored within the frame or automatically deploy for use. The ladder can be manual, semi-automatic, or remote controlled.

Abstract: An autonomous airborne carbon dioxide capturing assembly for carbon dioxide sequestration includes a plurality of airships each including a propulsion and navigation system, a sensor, and a carbon dioxide (CO2) capture and liquefaction module. The sensor measures CO2 concentrations. A computer is operationally engaged to the propulsion and navigation system, the sensor, the CO2 capture and liquefaction module, a positioning transceiver, and a communications transceiver. The computer automates decision-making and selectively actuates the propulsion and navigation system for controlled flight to a target area, to selectively actuate the CO2 capture and liquefaction module to capture and to liquefy CO2 from air at the target area, and to selectively actuate the propulsion and navigation system for controlled flight to a CO2 storage facility for offloading of the CO2.

Abstract: The present disclosure provides an augmented visual assessment system and methods of using the system for identification of a disorder in animals. In particular, the present disclosure provides an AVA (Augmented Visual Assessment) with CCS (Computed Core Symmetry) that allows practitioners to objectively gather, measure, assess and share data on gait asymmetry (e.g., lameness) and impaired motor movement of animals.

Abstract: Methods of treating superficial digital flexor tendon injuries, deep and superficial muscle/tendon contracture, navicular syndrome, and suspensory ligament inflammation and injuries in the limb of a quadruped animal, such as hooved animals and other quadrupeds. Such abnormalities may be inflammatory or associated with pain. The abnormalities may be chronic or acute. Such abnormalities may involve anatomical structures a limb, neck, torso, and/or pelvis of the quadruped animal.

Abstract: The invention provides a chemical-mechanical polishing composition comprising (a) an abrasive, (b) a cobalt accelerator, and (c) an oxidizing agent that oxidizes a metal, wherein the polishing composition has a pH of about 4 to about 10. The invention further provides a method of chemically-mechanically polishing a substrate with the inventive chemical-mechanical polishing composition. Typically, the substrate contains cobalt.

Abstract: An article of footwear including an upper and a sole structure. The sole structure includes a midsole, wherein the midsole includes an enclosed cavity, a thermoformed cushioning element disposed within the enclosed cavity, wherein the cushioning element includes an upper barrier film and a bottom barrier film enclosing an internal volume, and an outsole layer, wherein the outsole layer forms a ground-engaging surface of the article of footwear.

Abstract: A compound rotorcraft comprises a fuselage, a rotor coupled to the fuselage and a wing mounted to the fuselage. The rotorcraft further comprising a first outboard propeller, a first inboard propeller, a second outboard propeller, and a second inboard propeller. The first outboard propeller having a propeller body and propeller blades, the body mounted to a first wing-half at a first incidence angle. The first inboard propeller having a propeller body and propeller blades, the body mounted to the first wing-half between the first outboard propeller and the fuselage at a second incidence angle. The second outboard propeller having a propeller body and propeller blades, the body mounted to a second wing-half at a third incidence angle. The second inboard propeller comprising a propeller body and propeller blades, the body mounted to a second wing-half between the second outboard propeller in the fuselage at a fourth incidence angle.

Abstract: A system to prevent or limit resonance in a rotocraft. The system comprises an airframe, a rotor system having a natural frequency and including a rotor and a mast attached to the airframe, and a non-linear spring positioned between the rotor system and the airframe. The rotor system and the airframe are operable to move relative to each other as the rotor system begins to oscillate. The non-linear spring is configured to be deformed when the rotor system and the airframe move relative to each other such that the deformation of the non-linear spring causes the natural frequency of the rotor system to change. Also disclosed is a related method for preventing or limiting resonance in a rotorcraft.

Abstract: A system includes a sensor applicator, a sensor control device arranged within the sensor applicator and including an electronics housing and a sensor extending from a bottom of the electronics housing, and a cap coupled to one of the sensor applicator and the sensor control device, wherein the cap is removable prior to deploying the sensor control device from the sensor applicator.

Abstract: A system includes a sensor applicator, a sensor control device arranged within the sensor applicator and including an electronics housing and a sensor extending from a bottom of the electronics housing, and a cap coupled to one of the sensor applicator and the sensor control device, wherein the cap is removable prior to deploying the sensor control device from the sensor applicator.