Abstract: Frames for a head-mounted display may include a front frame portion, a facial interface portion with outer peripheral regions configured to flex to conform to a user's facial features when in use, and two upper support elements connecting the facial interface portion to the front frame portion. Intersection points between the upper support elements and the facial interface portion may be separated by a common interpupillary distance of expected users. Various other methods, head-mounted displays, frames and frame elements, and systems are also disclosed.

Abstract: Frame assemblies for a head-mounted display may include a facial interface frame, a display support frame, and at least one extendible tab coupled to the facial interface frame and the display support frame. The at least one extendible tab may be movable between a retracted position at which a near-eye display supported by the display support frame is located a first distance from the facial interface frame and a second position at which the near-eye display is located at a second, greater distance from the facial interface frame. Various other methods, head-mounted displays, frames and frame elements, and systems are also disclosed.

Abstract: The present disclosure relates to systems, non-transitory computer-readable media, and methods for automatically generating and executing machine learning pipelines based on a variety of user selections of various settings, machine learning structures, and other machine learning pipeline criteria. In particular, in one or more embodiments, the disclosed systems utilize user input selecting various machine learning pipeline settings to generate machine learning model pipeline files. Further, the disclosed systems execute and deploy the machine learning pipelines based on user-selected schedules. In some embodiments, the disclosed systems also register the machine learning pipelines and associated machine learning pipeline data in a machine learning pipeline registry. Further, the disclosed systems can generate and provide a machine learning pipeline graphical user interface for monitoring and managing machine learning pipelines.

Abstract: The present disclosure relates to systems, non-transitory computer-readable media, and methods that implement a pre-defined model container workflow allowing computing devices to flexibly and efficiently define, train, deploy, and maintain machine-learning models. For instance, the disclosed systems can provide scaffolding and boilerplate code for machine-learning models. To illustrate, boilerplate code can include predetermined designs of base classes for common use cases like training, batch inference, etc. In addition, the scaffolding provides an opinionated directory structure for organizing code of a machine-learning model. Further, the disclosed systems can provide containerization and various tooling (e.g., command interface tooling, platform upgrade tooling, and model repository management tooling). Additionally, the disclosed systems can provide out of the box compatibility with one or more different compute instances for increased flexibility and cross-system integration.

Abstract: A leading edge high-lift device, that may be deployable from a wing of an aircraft, may include a leading edge and a trailing edge. A lower surface and an upper surface may both extend between the leading edge and the trailing edge. A trailing edge region may be defined by the trailing edge and an adjacent region thereto. A shaping device may be disposed at the trailing edge region and may be movable between a non-activated position and an activated position.

Abstract: Rotor thrust balancing systems for turbomachines and methods of using the same are generally disclosed. For example, a rotor thrust balancing system for a turbomachine, wherein the turbomachine defines a centerline extending the length of the turbomachine. The system includes a rotating drive shaft, a thrust bearing, and a first waveguide sensor. The rotating drive shaft couples a turbine section and a compressor section of the turbomachine. The thrust bearing supports the rotating drive shaft of the turbomachine. The thrust bearing includes a plurality of ball bearings, an inner race coupled to the rotating drive shaft, and an outer race coupled to a fixed structure. The first waveguide sensor is coupled to the outer race at a first end of the waveguide sensor. The waveguide sensor communicates a vibrational frequency from the thrust bearing to a second end of the waveguide sensor.

Abstract: A casing for use in a turbofan engine is provided. The casing includes an inner hub, an intermediate casing positioned radially outward from the inner hub, an outer casing positioned radially outward from the intermediate casing, and a plurality of struts spaced circumferentially about the inner hub and extending between the inner hub and the outer casing. At least one strut of the plurality of struts includes a flow channel extending therethrough. The casing also includes a fluid scoop defined within the inner hub, and a collector that couples the fluid scoop in flow communication with the flow channel.

Abstract: Rotor thrust balancing systems for turbomachines and methods of using the same are generally disclosed. For example, a rotor thrust balancing system for a turbomachine, wherein the turbomachine defines a centerline extending the length of the turbomachine. The system includes a rotating drive shaft, a thrust bearing, and a first waveguide sensor. The rotating drive shaft couples a turbine section and a compressor section of the turbomachine. The thrust bearing supports the rotating drive shaft of the turbomachine. The thrust bearing includes a plurality of ball bearings, an inner race coupled to the rotating drive shaft, and an outer race coupled to a fixed structure. The first waveguide sensor is coupled to the outer race at a first end of the waveguide sensor. The waveguide sensor communicates a vibrational frequency from the thrust bearing to a second end of the waveguide sensor.

Abstract: A casing for use in a turbofan engine is provided. The casing includes an inner hub including a first fluid opening defined at bottom dead center of the casing. The casing also includes an intermediate casing positioned radially outward from the inner hub, an outer casing positioned radially outward from the intermediate casing, and struts spaced circumferentially about the inner hub and extending between the inner hub and the outer casing. The struts include a first strut and a second strut positioned on opposing sides of bottom dead center of the casing such that a first fluid sump is defined between the inner hub, the intermediate casing, and the first and second struts. At least one of said first and second struts includes a flow channel extending therethrough such that a fluid flow path is defined from the first fluid opening, through the first fluid sump, and through the flow channel.

Abstract: A leading edge high-lift device, that may be deployable from a wing of an aircraft, may include a leading edge and a trailing edge. A lower surface and an upper surface may both extend between the leading edge and the trailing edge. A trailing edge region may be defined by the trailing edge and an adjacent region thereto. A shaping device may be disposed at the trailing edge region and may be movable between a non-activated position and an activated position.

Abstract: A machine for non-woven fabric formation containing a rotating center shaft, at least a first and second pair of laterally spaced, interchangeable helical yarn guides, a yarn feeding wheel assembly, a fabric take up. The machine is capable of forming both square and tri-axial scrims with changes to the interchangeable helical yarn guides and yarn feeding wheel assembly.

Abstract: A machine for non-woven fabric formation containing a rotating center shaft, at least a first and second pair of laterally spaced, interchangeable helical yarn guides, a yarn feeding wheel assembly, a fabric take up. The machine is capable of forming both square and tri-axial scrims with changes to the interchangeable helical yarn guides and yarn feeding wheel assembly.

Abstract: A casing for use in a turbofan engine is provided. The casing includes an inner hub including a first fluid opening defined at bottom dead center of the casing. The casing also includes an intermediate casing positioned radially outward from the inner hub, an outer casing positioned radially outward from the intermediate casing, and struts spaced circumferentially about the inner hub and extending between the inner hub and the outer casing. The struts include a first strut and a second strut positioned on opposing sides of bottom dead center of the casing such that a first fluid sump is defined between the inner hub, the intermediate casing, and the first and second struts. At least one of said first and second struts includes a flow channel extending therethrough such that a fluid flow path is defined from the first fluid opening, through the first fluid sump, and through the flow channel.

Abstract: A leading edge high-lift device, that may be deployable from a wing of an aircraft, may include a leading edge and a trailing edge. A lower surface and an upper surface may both extend between the leading edge and the trailing edge. A trailing edge region may be defined by the trailing edge and an adjacent region thereto. A shaping device may be disposed at the trailing edge region and may be movable between a non-activated position and an activated position.

Abstract: A casing for use in a turbofan engine is provided. The casing includes an inner hub, an intermediate casing positioned radially outward from the inner hub, an outer casing positioned radially outward from the intermediate casing, and a plurality of struts spaced circumferentially about the inner hub and extending between the inner hub and the outer casing. At least one strut of the plurality of struts includes a flow channel extending therethrough. The casing also includes a fluid scoop defined within the inner hub, and a collector that couples the fluid scoop in flow communication with the flow channel.

Abstract: A window screen installation system is disclosed that includes a screen frame configured in a generally rectangular configuration from a plurality of screen frame extrusions. A plurality of trim molds are included that are configured to snap into place over the screen frame extrusion. When respective ends of the trim molds are positioned adjacent one another they form a plurality of generally rectangular shaped openings. A plurality of plinths are configured to be positioned in each of the plurality of openings configured to further secure the trim molds to the screen frame extrusions.

Abstract: A gazebo screen installation system is disclosed that is operable to allow screen frame assemblies to be installed in gazebos. The system includes a gazebo screen frame having a wedge portion and a trim portion. The trim portion includes a mounting rib extending upwardly from an upper surface of the trim portion and the wedge portion extends downwardly from said trim portion. A backing wedge strip is included having an angled surface and a mounting surface. The angled surface is formed in relation to the mounting surface such that a right angle forming angle is created in relation to a screen material when the backing wedge strip is connected with a vertical support member of a gazebo.

Abstract: A gazebo screen installation system is disclosed that is operable to allow screen frame assemblies to be installed in gazebos. The system includes a gazebo screen frame having a wedge portion and a trim portion. The trim portion includes a mounting rib extending upwardly from an upper surface of the trim portion and the wedge portion extends downwardly from said trim portion. A backing wedge strip is included having an angled surface and a mounting surface. The angled surface is formed in relation to the mounting surface such that a right angle forming angle is created in relation to a screen material when the backing wedge strip is connected with a vertical support member of a gazebo.