Abstract: A charge system includes a base, a platform including a projecting plug, at least three interlinked legs, and a first and second sets of articulating joints. The at least three interlinked legs are of a fixed same length and are mechanically biased to be perpendicular to the base. The first and second sets of articulating joints respectively connect opposite ends of the legs with the platform and base such that, responsive to a force on the plug, the legs tilt while remaining parallel to each other and the platform remains parallel with the base.

Abstract: A battery pack includes an enclosure assembly including a tray and a cover system secured relative to the tray. The cover system includes a first cover and a second cover that overlap one another. At least one of the first cover and the second cover includes a stepped design. Another battery pack includes an insert received within a tray and adapted to establish a first compartment and a second compartment within the tray. A first cover is positioned to cover the first compartment and a second cover is positioned to cover the second compartment.

Abstract: An exemplary support assembly includes a first housing that supports a first battery structure, a second housing that supports a second battery structure, a cover, and a common attachment that secures together the first housing, the second housing, and the cover. An exemplary support method includes securing together a first housing, a second housing, and a cover with a common attachment. The first housing supports a first battery structure that is enclosed by the second housing. The second housing supports a second battery structure that is enclosed by the cover.

Abstract: In one embodiment, a method includes receiving an indication that a user is interested in a content (e.g., newsfeed). Based on metadata associated with the content, a topic of the content and an entity associated with the content may be determined (e.g., a political candidate's position on gun control). One or more first entities (e.g., other political candidates) may be selected based on the entity associated with the content. The selected first entities may be different from the entity associated with the content. First contents associated with the first entities and topically related to the topic of the content may be selected (e.g., other candidates' positions on gun control). At least a portion of the first contents may be displayed with at least a portion of the content. The content and at least one of the first contents may have different sentiments toward the topic.

Abstract: One general aspect includes an electric vehicle (EV) high voltage (HV) battery pack cooling system, including: at least one battery cell positioned in a first compartment of a HV battery pack, where the first compartment is communicatively coupled to a cooling fluid inlet and a cooling fluid outlet positioned on the HV battery pack. The electric vehicle also includes a cooling fluid. The electric vehicle also includes a heat exchanger communicatively coupled to the cooling fluid inlet and the cooling fluid outlet.

Abstract: An exemplary method includes, among other things, winding a curable material at least partially about a plurality of battery cells that are compressed by a fixture. An exemplary assembly includes, among other things, a plurality of battery cells compressed by a fixture, and a curable material wound around the plurality of battery cells.

Abstract: A pedestal assembly receives a pylon assembly of a tiltrotor aircraft having an airframe including a fuselage and a wing. The pedestal assembly includes inboard and outboard tip ribs that extend above the wing and respectively define inboard and outboard slots. The pedestal assembly also includes inboard and outboard bearing cartridges. The inboard bearing cartridge is received within the inboard slot, is coupled to the inboard tip rib and includes an inboard bearing assembly. The outboard bearing cartridge is received within the outboard slot, is coupled to the outboard tip rib and includes an outboard bearing assembly. The inboard and outboard bearing assemblies are operable to receive the pylon assembly therein such that the pylon assembly is rotatably mounted between the inboard and outboard tip ribs to selectively operate the tiltrotor aircraft between a helicopter mode and an airplane mode.

Abstract: Opaque offerings of items conceal at least one attribute of the items from customers, typically a brand associated with the items. Such offerings usually include a generic description of the items and an opaque price that is typically lower than a standard offered price for the items. By identifying customers who may have an interest in such items, and tailoring opaque recommendations of such items to such customers, an online marketplace may increase the likelihood that such items will sell to customers while protecting an owner of a brand of such items from any negative implication or connotation that may be associated with offering such items at substandard prices.

Abstract: For an example method of reducing diffraction artifacts in a displayed image from a digital image projection system, a digital controller is coupled to a spatial light modulator. The spatial light modulator includes a two dimensional array of pixels. The method includes receiving signals containing pixel image data and processing the pixel image data to determine a desired gray scale for a pixel. The desired gray scale is compared to achievable gray scales of the digital image projection system. An upper bounding achievable gray scale is determined, and a lower bounding achievable gray scale is determined. Also, a dithering percentage for the desired gray scale is determined. The method chooses one of the upper bounding achievable gray scale and the lower bounding achievable gray scale. Also, a modified lower bounding gray scale is chosen to reduce the dithering percentage.

Abstract: A pedestal assembly for receiving a pylon assembly of a tiltrotor aircraft having a helicopter mode and an airplane mode, the tiltrotor aircraft having an airframe including a fuselage and a wing. The pedestal assembly includes an inboard pedestal supported by the airframe and positioned above the wing. The inboard pedestal includes an inboard bearing assembly disposed within an inboard pillow block housing. The pedestal assembly also includes an outboard pedestal supported by the airframe and positioned above the wing. The outboard pedestal includes an outboard bearing assembly disposed within an outboard pillow block housing. The inboard and outboard bearing assemblies are operable to receive the pylon assembly therein such that the pylon assembly is rotatably mounted between the inboard and outboard pedestals to selectively operate the tiltrotor aircraft between the helicopter mode and the airplane mode.

Abstract: System, method, and device for maximizing brightness of solid-state illuminators while minimizing power usage based on individual scene contents. An embodiment varies power to each of the solid-state illuminators (red, green, & blue) based on the scene content that is being displayed optimizing the non-linear brightness response of solid-state illuminators.

Abstract: In described examples, a method includes: receiving an array of image data pixels for display by a spatial light modulator; dividing the array of image data pixels into a plurality of blocks. For the blocks of the plurality of blocks, the method includes: computing a mean value for pixels in the block; computing a variance for pixels in the block; and, in response to the mean value and the variance, retrieving an indicator of a likelihood of a visible artifact for the block; and in response to the retrieved indicator, outputting a signal to selectively increase or reduce a load time of the spatial light modulator for displaying the array of image data pixels.

Abstract: In a method of image compression, a processor computes a palette for a block of pixels, the palette having palette values; and the processor computes index values, where some index values map a pixel to a palette value and some index values map a pixel to a value that is between two palette values.

Abstract: A propulsion system for a tiltrotor aircraft includes an engine supported by the airframe and a fixed gearbox operably coupled to the engine. Inboard and outboard pedestals are supported by the airframe and positioned above the wing. A pylon assembly is rotatably coupled between the inboard and outboard pedestals. The pylon assembly includes a spindle gearbox having an input gear, a mast operably coupled to the input gear and a proprotor assembly operable to rotate with the mast. The spindle gearbox is rotatable about a conversion axis to selectively operate the tiltrotor aircraft between helicopter and airplane modes. A common shaft, rotatable about the conversion axis, is configured to transfer torque from an output gear of the fixed gearbox to an input gear of the spindle gearbox. Each of the inboard and outboard pedestals includes a spherical bearing providing a self-aligning coupling with the pylon assembly.

Abstract: A pedestal assembly for receiving a pylon assembly of a tiltrotor aircraft having a helicopter mode and an airplane mode, the tiltrotor aircraft having an airframe including a fuselage and a wing. The pedestal assembly includes an inboard pedestal supported by the airframe and positioned above the wing. The inboard pedestal includes an inboard bearing assembly disposed within an inboard pillow block housing. The pedestal assembly also includes an outboard pedestal supported by the airframe and positioned above the wing. The outboard pedestal includes an outboard bearing assembly disposed within an outboard pillow block housing. The inboard and outboard bearing assemblies are operable to receive the pylon assembly therein such that the pylon assembly is rotatably mounted between the inboard and outboard pedestals to selectively operate the tiltrotor aircraft between the helicopter mode and the airplane mode.

Abstract: A propulsion system for a tiltrotor aircraft includes an engine supported by the airframe and a fixed gearbox operably coupled to the engine. Inboard and outboard pedestals are supported by the airframe and positioned above the wing. A pylon assembly is rotatably coupled between the inboard and outboard pedestals. The pylon assembly includes a spindle gearbox having an input gear, a mast operably coupled to the input gear and a proprotor assembly operable to rotate with the mast. The spindle gearbox is rotatable about a conversion axis to selectively operate the tiltrotor aircraft between helicopter and airplane modes. A common shaft, rotatable about the conversion axis, is configured to transfer torque from an output gear of the fixed gearbox to an input gear of the spindle gearbox. Each of the inboard and outboard pedestals includes a spherical bearing providing a self-aligning coupling with the pylon assembly.

Abstract: In described examples, a method includes: receiving an array of image data pixels for display by a spatial light modulator; dividing the array of image data pixels into a plurality of blocks. For the blocks of the plurality of blocks, the method includes: computing a mean value for pixels in the block; computing a variance for pixels in the block; and, in response to the mean value and the variance, retrieving an indicator of a likelihood of a visible artifact for the block; and in response to the retrieved indicator, outputting a signal to selectively increase or reduce a load time of the spatial light modulator for displaying the array of image data pixels.

Abstract: A battery pack includes a battery assembly including a grouping of battery cells and an integrated module attached to the grouping of battery cells. The integrated module includes an upper section housing at least one electronics component and a lower section establishing a vent chamber.

Abstract: A battery pack includes an enclosure assembly including a tray and a cover system secured relative to the tray. The cover system includes a first cover and a second cover that overlap one another. At least one of the first cover and the second cover includes a stepped design. Another battery pack includes an insert received within a tray and adapted to establish a first compartment and a second compartment within the tray. A first cover is positioned to cover the first compartment and a second cover is positioned to cover the second compartment.

Abstract: A battery pack includes a first side oriented battery assembly, a second side oriented battery assembly, and a vent chamber arranged between the first side oriented battery assembly and the second side oriented battery assembly. The first and second side oriented battery assemblies are thus arranged to share a common vent chamber. One of the first and second side oriented battery assemblies may additionally share a common heat exchanger device with a third side oriented battery assembly.