A tool for fabrication of a thermoplastic panel includes a sealed vessel, a membrane and a heater. The sealed vessel defines a volume. The sealed vessel includes first and second fluid ports. The membrane is disposed within the volume to define first and second chambers. The first chamber receives a skin and a core of the thermoplastic panel. The first chamber selectively applies a first fluidic pressure to the skin and the core in response to receiving a first fluid via the first fluid port. The membrane abuts a major surface of the thermoplastic panel. The second chamber selectively applies a second fluidic pressure to the membrane in response to receiving a second fluid via the second fluid port. The heater selectively directs heat toward the first chamber. A method for fabrication of the thermoplastic panel is provided. Various examples of thermoplastic panels are also provided.

A method of forming a thermoplastic cellular structure includes positioning a lower surface of a trough of a first corrugated thermoplastic sheet against an upper surface of a crest of a second corrugated thermoplastic sheet; positioning a support against a lower surface of the crest of the second corrugated thermoplastic sheet; and pressing a thermoplastic welding element against an upper surface of the trough of the first corrugated thermoplastic sheet so that at least a portion of the lower surface of the trough of the first corrugated thermoplastic sheet melts and bonds to at least a portion of the upper surface of the crest of the second corrugated thermoplastic sheet.

The present invention is related to a process for bordering a corrugated plastic panel and to a panel obtained through that process. In particular, the invention is related to a process for making a corrugated plastic panel comprising a bordering made in-line or out-line in order to close the openings outwards. The invention is also related to an apparatus for bordering according to that process. The panel is sealed and shock resistant thanks to the laying of thermoplastic elastomeric material.

A printing method for printing a multi-material 3D model comprises the following steps: perform a slicing process on a multi-material 3D object to generate the multi-material object slices and the object slices of a useful object; compute a material-switching point and a retrieving point during the slicing process; print the multi-material object slices of a multi-material 3D model with one of the materials; when print to the material-switching point, switch to another different material and print useful objects with the material used before the material switching; when print to the retrieving point, print the multi-material object slices with the material used after the material switching; and repeat the above steps until completing the multi-material 3D model printing. The present disclosed example prints the useful object via the remaining materials after the material switching which effectively reduces the cost with of multi-materials printing.

The present invention sufficiently heats a repairing material while preventing change in quality of a base material provided with the repairing material so as to securely bond the repairing material to a repair target portion. The repair method of the present invention, in order to repair a repair target portion 14 existing in an outer panel 1, includes: a repairing material disposing step of disposing a repairing patch 21 including a resistance heating element 23 and a carbon fiber reinforced resin, and an adhesive 22A including a thermosetting resin before being hardened for bonding the repairing patch 21 on the repair target portion 14; and a heating-hardening step of heating and hardening the thermosetting resin of the adhesive 22A by causing the resistance heating element 23 to generate heat through supply of electricity thereto.

A method of fastening an edge structure to a construction element includes providing the construction element, being a planar structure with with two cover regions and a middle region between the cover regions; providing the edge structure being continuously extended, the edge structure having contact surfaces with a thermoplastic material shaped to lie against the cover regions in an outer surface of the construction element, and, opposite the contact surfaces, a coupling-in surface for coupling energy into the edge structure; coupling energy into the edge structure and pressing the contact surfaces against the cover regions until at least a portion of the thermoplastic material is liquefied and pressed into the cover regions; and repeating or continuing the steps of coupling and pressing until the edge structure is attached to the building element at a plurality of discrete locations or over an extended region along an edge of the construction element.

A component, including a part, comprising a honeycomb-like structure formed from at least a seamless resin-infused fiber composite material. The honeycomb-like structure includes a first plurality of honeycomb-like cells, and a second plurality of honeycomb-like cells, different than the first plurality of honeycomb-like cells.

Packages used to deliver items or other payloads via a drone may be customized and 3D printed to house the payload. The package may be customized to minimize the size and/or weight needed to house the payload. The customized packages may include one or more attachment mechanisms adapted to engage with or otherwise be coupled to the drone for delivery. Multiple individual customized packages can be secured together into a composite package for delivery by drone. The customized package may be designed to be aerodynamic given the shape of the payload and the flight characteristics of the drone. The drone itself may be the package, with the payload housed within a portion of the drone. The package and/or a portion of the drone (e.g., fuselage, wing, body, frame, etc.) may be printed at least partially in, on, or around an item or package to be transported by the drone.

Provided are splices comprising honeycomb cores and adhesive layers with tie clips supporting the honeycomb cores. Also provided are methods of forming such splices. Each tie clip includes two legs and a bridging portion joining the legs. When forming a splice, an adhesive layer is positioned between two honeycomb cores. One leg of the tie clip is inserted into the full cell of one honeycomb core, while the other leg is inserted into the full cell of the other honeycomb core. The bridging portion extends across the adhesive layer. While curing the adhesive layer, the tie clip supports the honeycomb cores with respect to each other and maintains their orientation. The tie clip becomes a part of the splice. The tie clip may be buried in the honeycomb cores without extending above the first face of the splice.

Methods and apparatus for a head covering may improve air circulation through any suitable head covering. Methods and apparatus for a head covering may comprise a base configured to fit around a wearer's head, a sidewall comprising a plurality of open cells configured to prevent light rays at or above a predetermined angle relative to the passageway of each cell from passing unobstructed through the cell, and a crown configured to close of the interior surface of the sidewall. The minimum depth of each cell may be determined based on the height of the cell, the angle at or above which the light rays are to obstructed, and the angle of the exterior cell opening. The cells may be arranged in the sidewall such that the lower surface of the passageway of each cell is substantially at the same angle with respect to a horizontal plane.