Abstract: Systems, methods, and apparatus for multifunctional battery packaging and insulation are disclosed. In one or more embodiments, a battery pack comprises a plurality of battery cells. The battery pack further comprises a block comprising a plurality of recesses formed within the block. In one or more embodiments, each of the recesses respectively houses one of the battery cells within the block. In at least one embodiment, the block comprises a low density ceramic fiber reinforced foam that is porous such that a gas or liquid may pass through the block to cool the battery pack. In one or more embodiments, at least a portion of the block is covered with a ceramic matrix composite (CMC) material comprising a ceramic slurry composite pre-impregnated (prepreg) with fibers. In some embodiments, the CMC material is cured via kiln firing the block.

Abstract: Methods and systems, and components made according to the methods and systems, are disclosed relating to improved methods for fabricating resin-containing composite prepreg materials, wherein the prepreg plies are treated with a particulate material to achieve predetermined spatially variable shear and tack values at a predetermined location on at least one prepreg ply surface of at least one prepreg ply.

Abstract: Systems, methods, and apparatus for multifunctional battery packaging and insulation are disclosed. In one or more embodiments, a battery pack comprises a plurality of battery cells. The battery pack further comprises a block comprising a plurality of recesses formed within the block. In one or more embodiments, each of the recesses respectively houses one of the battery cells within the block. In at least one embodiment, the block comprises a low density ceramic fiber reinforced foam that is porous such that a gas or liquid may pass through the block to cool the battery pack. In one or more embodiments, at least a portion of the block is covered with a ceramic matrix composite (CMC) material comprising a ceramic slurry composite pre-impregnated (prepreg) with fibers. In some embodiments, the CMC material is cured via kiln firing the block.

Abstract: Methods and systems, and components made according to the methods and systems, are disclosed relating to improved methods for fabricating resin-containing composite prepreg materials, wherein the prepreg plies are treated with a particulate material to achieve predetermined spatially variable shear and tack values at a predetermined location on at least one prepreg ply surface of at least one prepreg ply.

Abstract: Systems and methods for controlling an overhead gantry crane are provided. One overhead gantry crane includes an X-axis drive motor, a Y-axis drive motor, and a hoist member operable to be moved into a plurality of positions by the X-axis drive motor and the Y-axis drive motor to move an object. The overhead gantry crane further includes a controller operable to control operation of the X-axis motor and the Y-axis motor and define a local axis coordinate system for the overhead gantry crane based on a reference point determined from an X-axis location and Y-axis location of the hoist member and a desired movement path for the object, as well as cause movement of the object by concurrently controlling the X-axis motor and the Y-axis motor using the local axis coordinate system.

Abstract: Systems and methods of reproducing images onto surfaces are disclosed. In one embodiment, the system includes an image file that digitally produces a planar surface normal to a surface of a master model. The planar surfaces are referenced to a coordinate system of the master model through a series of points. A tracker surfacing system, comprising a tracking instrument, generates and emits a signal as the tracking instrument crosses the planar surface. An output device is actuated by the tracking device as it crosses the planar surface, reproducing the series of points as an image onto a surface, including a flat, curved or compound surface. Both the spatial position and orientation of the output device are detected and adjustments are made so that the image is precisely applied to intended locations on the surface being imaged.

Abstract: A method for depositing a substance on a real surface of a real object comprises tracking position of an output device on the real surface as the output device is being moved over the real surface. The output device includes a substance-depositing device. The method further comprises using a computer-generated representation of the real surface and extruded surfaces normal to the representation surface at locations where the substance should be deposited; indicating a corresponding tracked position of the output device on the representation surface; and commanding the output device to deposit a substance on the real surface whenever the tracked position on the representation surface crosses an extruded surface.

Abstract: A method for making a honeycomb composite structure wherein the method allows for fluid flow from cells of a honeycomb core during a cure process. More specifically, the method involves forming one or more vents in a skin of the structure, which are preferably filled with venting wicks, to allow for fluid flow before being sealed by the polymer matrix during a skin bonding process. Additionally, the structure preferably comprises a scrim that allows for fluid flow between multiple cells of the honeycomb core. The honeycomb composite structure produced according to this process comprises, among other things, a sealed venting region that comprises a polymer matrix and fibers that are transverse to the skin.

Abstract: The present application is directed to systems for controlling the direction of thermal expansion of a composite part during thermal processing. The systems may comprise at least one guiding mechanism capable of being attached to a surface of a tool for fabricating composites and at least one moveable composite insert capable of being attached to a composite part. The moveable composite insert has an opening for receiving the at least one guiding mechanism. The opening is capable of controlling movement of the at least one moveable composite insert in a desired direction during thermal expansion of the composite part, when the guiding mechanism is received by the opening. Methods for controlling the direction of thermal expansion of a composite part during thermal processing are also disclosed.

Abstract: The present application is directed to systems for controlling the direction of thermal expansion of a composite part during thermal processing. The systems may comprise at least one guiding mechanism capable of being attached to a surface of a tool for fabricating composites and at least one moveable composite insert capable of being attached to a composite part. The moveable composite insert has an opening for receiving the at least one guiding mechanism. The opening is capable of controlling movement of the at least one moveable composite insert in a desired direction during thermal expansion of the composite part, when the guiding mechanism is received by the opening. Methods for controlling the direction of thermal expansion of a composite part during thermal processing are also disclosed.

Abstract: The present application is directed to systems for controlling the direction of thermal expansion of a composite part during thermal processing. The systems may comprise at least one guiding mechanism capable of being attached to a surface of a tool for fabricating composites and at least one moveable composite insert capable of being attached to a composite part. The moveable composite insert has an opening for receiving the at least one guiding mechanism. The opening is capable of controlling movement of the at least one moveable composite insert in a desired direction during thermal expansion of the composite part, when the guiding mechanism is received by the opening. Methods for controlling the direction of thermal expansion of a composite part during thermal processing are also disclosed.

Abstract: An annular core cutting apparatus includes a cutting head including a generally cylindrical sidewall having a first end and a second end, wherein the first end has a cutting edge, and wherein the sidewall includes a plurality of openings having at least one sharpened edge. A spindle is coaxially and rigidly coupled to the second end of the cylindrical sidewall, and the spindle configured to rotate about a rotational axis. In a further embodiment, a generally conical member is disposed within the cutting apparatus to assist with grinding and removal of waste material.

Abstract: An annular core cutting apparatus includes a cutting head including a generally cylindrical sidewall having a first end and a second end, wherein the first end has a cutting edge, and wherein the sidewall includes a plurality of openings having at least one sharpened edge. A spindle is coaxially and rigidly coupled to the second end of the cylindrical sidewall, and the spindle configured to rotate about a rotational axis. In a further embodiment, a generally conical member is disposed within the cutting apparatus to assist with grinding and removal of waste material.

Abstract: Honeycomb products and methods of manufacture thereof, particularly for aerospace applications. The honeycomb core products are made of a plastic material, such as a thermoplastic material, and preferably are made by a direct manufacturing process, such as stereo lithography, selective laser sintering, or fused deposition modeling. The cell sizes, shapes and wall thicknesses can be modified or varied throughout the product as desired. An interlocking structure is utilized to securely hold together adjacent honeycomb products.