A vacuum insulation assembly for an appliance includes a plurality of panels that define a cavity. Each of the plurality of panels includes an inner surface. A port opening is defined by one of the plurality of panels and is defined in communication with the cavity. A vacuum insulation material is positioned within the cavity. A stiffening material is coupled to the inner surface of one or more of the plurality of panels. The stiffening material includes a polymer layer configured to adhere to the inner surface when the stiffening material is heated. A mesh layer is positioned over the polymer layer.

A vehicle interior part includes a substrate, a first outer layer, a second outer layer, an upper reinforcement layer, a lower reinforcement layer, and a bottom fabric layer, where a first surface and a second surface of the substrate are bonded to a first surface of the upper reinforcement layer and a first surface of the lower reinforcement layer, respectively, a second surface of the upper reinforcement layer is bonded to a first surface of the first outer layer, a second surface of the first outer layer is bonded to the second outer layer, and a second surface of the lower reinforcement layer is bonded to the bottom fabric layer.

An aircraft body section comprises a first layer of composite material, a first group of conductive traces, a second layer of composite material, and a first group of conductive connectors. The first layer of composite material has an upper surface and a lower surface, with the lower surface forming an exterior surface of a body of the aircraft. The first group of conductive traces are formed on the upper surface of the first layer of composite material. The second layer of composite material is positioned on the first layer of composite material and has an upper surface and a lower surface, with the upper surface forming an interior surface of a body of the aircraft. The first group of conductive connectors is formed on the upper surface of the second layer of composite material and is configured to provide electrical connection from external conductors to the conductive traces.

An aircraft body section comprises a first layer of composite material, a first group of conductive traces, a second layer of composite material, and a first group of conductive connectors. The first layer of composite material has an upper surface and a lower surface, with the lower surface forming an exterior surface of a body of the aircraft. The first group of conductive traces are formed on the upper surface of the first layer of composite material. The second layer of composite material is positioned on the first layer of composite material and has an upper surface and a lower surface, with the upper surface forming an interior surface of a body of the aircraft. The first group of conductive connectors is formed on the upper surface of the second layer of composite material and is configured to provide electrical connection from external conductors to the conductive traces.

A fluid impervious wall skin provides an interstitial space. The wall is formed from a composite material, the composite material comprising a plurality of layers including:, a first layer of flexible material having adhesive on at least one surface thereof for attachment to a structural wall; a layer comprising a spacer; and a second layer of flexible material; the layers of the composite material are attached a structural wall and one to the other by adhesive between adjacent layers, and the spacer provides the interstitial space N between the said first and second layers of flexible material within the said composite material. The second flexible layer comprises heavier than the second weight, wherein the each overlapping sheet presents a free edge, and the tape is positioned over the free edge is attached to the overlapping and the overlapped sheet of woven fibreglass fabric of the first weight, and a solvent free epoxy coating applied to the surface of the second flexible layer that is distal from the structural wall, which coating cures to form a hard fluid impervious layer.

Disclosed is a heat insulator comprising a substrate comprising of a bulk of silica-based inorganic fiber containing a hydroxyl group; a metallic or ceramic infrared mediator held on at least a part of one surface of the substrate; and a silica cured product holding the infrared mediator on/in the substrate. As the infrared mediator, a metal foil or a ceramic particle may be used. This heat insulator exhibits excellent heat insulating performance in a high temperature range of 600° C. or more, and can be molded into a three-dimensional shape which can be directly mounted to a structure.

Disclosed is a heat insulator comprising a substrate comprising of a bulk of silica-based inorganic fiber containing a hydroxyl group; a metallic or ceramic infrared mediator held on at least a part of one surface of the substrate; and a silica cured product holding the infrared mediator on/in the substrate. As the infrared mediator, a metal foil or a ceramic particle may be used. This heat insulator exhibits excellent heat insulating performance in a high temperature range of 600° C. or more, and can be molded into a three-dimensional shape which can be directly mounted to a structure.

A method of using a self-stick insulation. The method includes providing a piece of insulation product with an adhesive coating. The adhesive coating includes polystyrene-maleic anhydride (SMA) and/or polyacrylic acid (PAA); an alcohol amine; and at least one of a polyvinyl alcohol and a starch. The adhesive coating is then activated with liquid water. Once the adhesive coating is active, the insulation product is attached to a surface with the adhesive coating.

A method of using a self-stick insulation. The method includes providing a piece of insulation product with an adhesive coating. The adhesive coating includes polystyrene-maleic anhydride (SMA) and/or polyacrylic acid (PAA); an alcohol amine; and at least one of a polyvinyl alcohol and a starch. The adhesive coating is then activated with liquid water. Once the adhesive coating is active, the insulation product is attached to a surface with the adhesive coating.

A fibrous insulation product having a plurality of randomly oriented glass fibers and a binder composition that holds the glass fibers together is disclosed. The fibrous insulation product has an R-value in the range of 10 to 54 and, after curing, has a density, when uncompressed, in the range of 0.30 pcf to 2.7 pcf. Furthermore, the fibrous insulation product includes glass fibers that, prior to the application of the binder composition, have an average fiber diameter in the range of 15 HT to 19 HT and a quantity of binder that is in the range of 2% to 10% by weight of the fibrous insulation product. The fibrous insulation product also has an average fiber diameter to density ratio (Fd/D) of less than or equal to 40 and a comfort factor less than or equal to 3.417(Fd/D)+60.