Abstract: A releasable connection for coiled tubing drilling apparatus is presented wherein the connection has an outer body configured with an inner volume, a mandrel located at least partially within the outer body and in the inner volume, a plug located with the outer body and a structural weakpoint apparatus, wherein the structural weakpoint apparatus is configured to structurally fail at a predetermined tensile load placed upon the releasable connection apparatus, wherein the structural weakpoint apparatus is configured at a lower end of the mandrel.

Abstract: A method of repairing an oxidized defect in a superalloy article includes removing substantially all of the oxidized defect to form a cleaned out portion of the superalloy article; filling a portion of the cleaned out portion with a weld by fusion welding; cracking the weld; and filling the cracked weld and a remaining portion of the cleaned out portion with a braze material.

Abstract: A system for inspecting a turbomachine includes a traverse actuator system having a carriage configured to move a probe into and out of the turbomachine. The traverse actuator system has a track with a plurality of linearly arranged teeth. The track is configured for operation with the carriage. A motor is operably connected with the carriage and track, and the motor is configured to engage the plurality of linearly arranged teeth so that operation of the motor forces the carriage to move along the track.

Abstract: A method for inspecting a turbomachine is provided. The method includes the steps of, attaching a gimbal mount to the turbomachine, inserting a probe into the turbomachine through the gimbal mount, and adjusting a position of the probe via the gimbal mount. A removing step removes the probe from the turbomachine. An attaching step attaches a traverse actuator system to the gimbal mount. The traverse actuator system is connected to the gimbal mount through a pressure isolation system. A reinserting step is used to reinsert the probe back into the turbomachine. An inspecting step is used to inspect or test the turbomachine.

Abstract: The brake cylinder comprises a cylinder body comprising an annular flange and a non-pressure head. The annular flange of the cylinder body defines a plurality of openings. The non-pressure head has an annular flange and a head portion extending from the annular flange. The annular flange of the non-pressure head has a plurality of bosses and a plurality of openings corresponding to and aligned with the plurality of openings in the annular flange of the cylinder body. At least one vent is positioned in one of the plurality of bosses. The cylinder body and the non-pressure head are secured to each other at the respective flanges. The vent is positioned in the boss disposed opposite a mounting portion so that when the brake cylinder is mounted to a railway vehicle, the vent is oriented in a bottom position on the cylinder body with respect to a ground surface.

Abstract: A system for inspecting a turbomachine is provided. The system includes a pressure isolation system configured to maintain a pressure resistant seal around a probe. The pressure isolation system has a probe bearing located adjacent to a pressure seal. The probe bearing is configured to facilitate back and forth movement of the probe by reducing friction. A gimbal mount is connected to the pressure isolation system. The pressure isolation system has a valve seal located between the gimbal mount and the pressure seal. The valve seal is configured to isolate the pressure seal from the gimbal mount when the probe is not in the valve seal. The system is configured to move the probe into and out of the turbomachine.

Abstract: A method for removing oxide from a metallic substrate is described. The method includes providing a stream of boron trifluoride; heating the metallic substrate at a first temperature; and heating the metallic substrate at a second temperature different from the first temperature. An associated apparatus is also described.

Abstract: An article treatment method is disclosed including removing an affected area from an article, the article including the affected area and a substrate composed of a substrate material, forming an unaffected surface. A structural material is applied to the unaffected surface by cold spraying a plurality of particles of the structural material from a cold spray apparatus. The structural material and the article are finished, forming a treated article including an unused article conformation. A turbine component treatment method is disclosed for a turbine component including a hard-to-weld (HTW) alloy, wherein applying the structural material includes impacting the plurality of particles, and plastically deforming the plurality of particles to form a mechanical bond between the structural material and the HTW alloy. An airfoil treatment method is disclosed further including the cold spraying forming a near net shape of an unused airfoil composition.

Abstract: This invention relates to novel extended release pharmaceutical compositions of levetiracetam and preparations and characterizations thereof. This invention further relates to using these extended release pharmaceutical compositions of levetiracetam for the treatment of cognitive impairment associated with central nervous system (CNS) disorders in a subject in need or at risk thereof.

Abstract: A panel structure having a low-density core that can withstanding loads normal to a first primary surface, and a first facing of high-density sheet material that can extend along the first primary surface. The high-density sheet material can be laminated on the core such that the laminated core and facing cooperatively resist bending loads and loads along the primary surface. The first facing can extend from the first primary surface on a side of the core along a secondary surface, which can be non-parallel to the first primary surface. The first facing can bend along a score line between the first primary surface and the secondary surface.

Abstract: In one general aspect, a method of coupling a base to a lid of a computing device using a hinge can include coupling a base hinge flange to the base, the base hinge flange being connected to a base hinge part that includes a knuckle including a toggle pivot, the toggle pivot coupled to and surrounding a first portion of a first shaft, and coupling a lid hinge flange to the lid, the lid hinge flange being connected to a main hinge part that includes a first cam, the lid hinge flange including a first lid main band and a second lid main band surrounding a first portion of a second shaft, the second shaft being parallel to the first shaft.

Abstract: A high efficiency evaporative toilet provides a unique air introduction and exposure/utilization system providing a unique air flow pattern that draws hot air over solids and then over liquids for absorption of moisture in three different technological options. An expansion of the liquid surface exposed to hot air is achieved through the use of wicking in the carousel and microwave applications. An air exhaust system provides a unique exhaust flow system that draws saturated air out of the system and is operated nonstop, using minimal amounts of electricity with the added option of being compatible with the use of solar panels.

Abstract: A system for inspecting a turbomachine is provided. The system includes a traverse actuator system and a pressure isolation system connected to the traverse actuator system. The pressure isolation system is configured to maintain a pressure resistant seal around a probe. A gimbal mount is connected to the pressure isolation system. The system is configured to move the probe into and out of the turbomachine.

Abstract: A method for inspecting a turbomachine is provided. The method includes the steps of, attaching a gimbal mount to the turbomachine, inserting a probe into the turbomachine through the gimbal mount, and adjusting a position of the probe via the gimbal mount. A removing step removes the probe from the turbomachine. An attaching step attaches a traverse actuator system to the gimbal mount. The traverse actuator system is connected to the gimbal mount through a pressure isolation system. A reinserting step is used to reinsert the probe back into the turbomachine. An inspecting step is used to inspect or test the turbomachine.

Abstract: A system for inspecting a turbomachine is provided. The system includes a pressure isolation system configured to maintain a pressure resistant seal around a probe. The pressure isolation system has a probe bearing located adjacent to a pressure seal. The probe bearing is configured to facilitate back and forth movement of the probe by reducing friction. A gimbal mount is connected to the pressure isolation system. The pressure isolation system has a valve seal located between the gimbal mount and the pressure seal. The valve seal is configured to isolate the pressure seal from the gimbal mount when the probe is not in the valve seal. The system is configured to move the probe into and out of the turbomachine.

Abstract: A system for inspecting a turbomachine includes a traverse actuator system having a carriage configured to move a probe into and out of the turbomachine. The traverse actuator system has a track with a plurality of linearly arranged teeth. The track is configured for operation with the carriage. A motor is operably connected with the carriage and track, and the motor is configured to engage the plurality of linearly arranged teeth so that operation of the motor forces the carriage to move along the track.

Abstract: Systems, methods and devices for paired training include timing controls so that training and neural stimulation can be provided simultaneously. Paired trainings may include therapies, rehabilitation and performance enhancement training. Stimulations of nerves such as the vagus nerve that affect subcortical regions such as the nucleus basalis, locus coeruleus or amygdala induce plasticity in the brain, enhancing the effects of a variety of therapies, such as those used to treat tinnitus, stroke, traumatic brain injury and post-traumatic stress disorder.

Abstract: A releasable connection for coiled tubing drilling apparatus is presented wherein the connection has an outer body configured with an inner volume, a mandrel located at least partially within the outer body and in the inner volume, a plug located with the outer body and a structural weakpoint apparatus, wherein the structural weakpoint apparatus is configured to structurally fail at a predetermined tensile load placed upon the releasable connection apparatus, wherein the structural weakpoint apparatus is configured at a lower end of the mandrel.

Abstract: A reconfigurable advanced rapid-prototyping environment (RARE) solution provides a three-dimensional (x, y, z) interconnection fabric that is a modular, reconfigurable, fully scalable high performance computing architecture. RARE allows processing nodes (modules) to communicate with other processing nodes (modules) in a three-dimensional mesh architecture where every processing node (module) has access to all other nodes (modules) in the system. The RARE architecture is a modular form-factor design which is fully stand-alone. It does not require the use of a backplane or chassis infrastructure for connectivity. RARE is widely scalable and provides full cross-channel communication in all three dimensions (x, y, z). RARE yields a scalable and morphable hardware architecture for a processing system where the system can scale by one module at a time without limit and it can take on any shape and those shapes can be easily changed.