A shower pan and method of manufacture are described. Embodiments of the shower pan can include, but are not limited to, a solid surface top layer and a PET second layer that can be thermoformed, molded, and laminated in a single step. The solid surface top layer can be approximately ⅛″ to ¼″ thick and the PET second layer can be approximately ⅞″ to 1⅛″ thick. The shower pan may further include a third layer being fiberglass.

The present disclosure relates generally to cladding for covering a building surface, for example suitable for covering the exterior surface of a building. The present disclosure relates more particularly to a siding panel including a panel body having a length, a width, a front face, and a rear face. The panel body further includes a first strip extending along the length of the panel body with a three dimensional surface texture. The three dimensional surface texture is a geometric pattern repeating along the front face of the panel body. The panel body includes a second strip extending along the length of the panel body adjacent to the first strip with a surface texture that is different than that of the first strip. The siding panel further includes a first lock, a second lock, and a fastening strip secured to the first lock.

The invention disclosed herein is an automotive acoustic panel including a porous sound-absorption material made from a polymer and an expanded perlite. One or more silane compounds may be coupled or coated onto the expanded perlite while a coupling agent and a chemical foaming agent may additionally be added to the automotive acoustic panel.

Object: Provided is a decorative vapor deposition sheet that can reduce or prevent a defect, such as the breaking of a metal vapor deposition layer or the entire sheet, even when applied to a forming method requiring high temperature or the like. The decorative vapor deposition sheet of an embodiment of the present disclosure is a decorative vapor deposition sheet including a cover resin layer and a metal vapor deposition layer, in which the cover resin layer has a thickness of approximately 50 micrometers or greater, the metal vapor deposition layer exhibits a granular structure, a breaking elongation of the decorative vapor deposition sheet at 20° C. is approximately 120% or greater, and a breaking elongation of the decorative vapor deposition sheet at 160° C. is approximately 350% or greater.

A frame for a lightweight costume with air permeability, the costume, and a method for manufacturing them. The frame body for the costume includes a main body made of synthetic resin and a plurality of through holes penetrating the main body. The method includes a mold installation step of installing a mold in a predetermined three-dimensional shape on an elevating table, a resin member mounting step of mounting a resin member on a pedestal, a cover mounting step of mounting a cover covering the surface of the resin member on the pedestal, a heating step of heating the resin member and the cover, a vacuum molding step of bringing the mold into contact with the back surface of the resin member and then depressurizing the inside of the chamber, and a mold release step of releasing the frame body and the cover from the mold.

This thermoforming machine includes a thermoforming chamber having at least one heated air inlet through which heated air flows into the thermoforming chamber at a controlled pressure. The air inlet cooperates with a heated air flow distribution regulator located in the thermoforming chamber and through which the heated air flows out of the thermoforming chamber at a predetermined temperature. The regulator includes a heated air flow regulating mask receiving heated air flow, having a plurality of flow restricting elements providing different air flow restrictions.

A frame is injection molded onto a group of panels to form a container. The panels extend at least partially around, and at least partially define, a cavity of the container.

A method for molding a composite pressure vessel liner to secure a boss to the liner is described. The method comprises providing a moldable liner having an end section with a neck and a port. A boss is positioned around the neck of the liner and the liner is heated and pressure is applied to mold the liner to form to the shape of the boss. The angle of the molded liner secures the boss in place around the liner and it is able to withstand high pressures. A tool for molding the liner and a method for using the tool is also described. The tool comprises a tool body and a pipe having external threads. The tool body abuts the liner and the boss. Winding the pipe exerts pressure on the liner, which when heated, forces the liner to mold to the shape of the boss.

A method for molding a composite pressure vessel liner to secure a boss to the liner is described. The method comprises providing a moldable liner having an end section with a neck and a port. A boss is positioned around the neck of the liner and the liner is heated and pressure is applied to mold the liner to form to the shape of the boss. The angle of the molded liner secures the boss in place around the liner and it is able to withstand high pressures. A tool for molding the liner and a method for using the tool is also described. The tool comprises a tool body and a pipe having external threads. The tool body abuts the liner and the boss. Winding the pipe exerts pressure on the liner, which when heated, forces the liner to mold to the shape of the boss.

A thermal/acoustic insulation product, such as for an aircraft, comprising a block of flexible, open-celled, cellular foam having a predefined shape and having a thermoformed amorphous film covering that completely envelops the foam block. A process for making the insulation product includes first cutting the block of foam to a predefined shape, such as a shape suitable for placement in an area of an aircraft in need of insulation. Then, a first sheet of film is heated to its melt point and conformed to a first surface area of the block, and a second sheet of film is heated to its melt point and conformed to a second surface area of the block, wherein the first film and the second film are joined to one another at one or more seams. The insulation product may then be installed in an aircraft.