B32B37/30

PRESSED LAMINATE PANEL WITH A SINGLE LAYER ELASTOMERICK TREATED PAPER
20180222169 · 2018-08-09 ·

A laminated panel is provided which comprises, or consists of, a core panel to which an elastomeric resin impregnated single finishing printed paper layer has been applied. The paper for the single finishing printed paper layer is printed to provide a design feature on the laminated panel. Preferably, the design feature has been printed on a lower surface of the single finishing printed paper layer. As a result of the resin impregnation and heating and pressing operations, the single finishing printed paper layer becomes translucent or transparent, and thus allows the printed design feature to become visible. The design feature can be printed onto the single finishing printed paper prior to treatment with the elastomeric resin, or printed onto the previously treated elastomeric resin impregnated paper. The laminated panels can be used in the production of laminated flooring, wall panels or furniture panels.

Prepregs Including UV Curable Resins Useful for Manufacturing Semi-Flexible PCBs
20180200992 · 2018-07-19 ·

Prepregs having a UV curable resin layer located adjacent to a thermally curable resin layer wherein the UV curable resin layer includes at least one UV cured resin portion and at least one UV uncured resin as well as methods for preparing flexible printed circuit boards using the prepregs.

Optical window system with aero-optical conductive blades

A method of improving optical characteristics of an optical window operating in a flow of fluid and having first and second panes of optically transmissive materialeach having an edge adjacent to, parallel with, and at least partially coextensive with each otheris described herein. The method includes inserting a thermally conductive blade between two adjacent edges of the first and second panes of optically transmissive material; and lifting an adverse flow stagnation zone forward of the optical window by protruding the thermally conductive blade into the flow of fluid from an outer surface of the panes of the optical window.

Optical window system with aero-optical conductive blades

A method of improving optical characteristics of an optical window operating in a flow of fluid and having first and second panes of optically transmissive materialeach having an edge adjacent to, parallel with, and at least partially coextensive with each otheris described herein. The method includes inserting a thermally conductive blade between two adjacent edges of the first and second panes of optically transmissive material; and lifting an adverse flow stagnation zone forward of the optical window by protruding the thermally conductive blade into the flow of fluid from an outer surface of the panes of the optical window.

LAMINATED ARTICLES AND METHODS OF MAKING AND USING THE SAME
20180125127 · 2018-05-10 ·

Described herein are laminated articles along with methods of making and/or using the same, including a continuous process for making laminated articles.

Method for making multi-ply fibrous structures

Embossed multi-ply fibrous structures and methods for making such embossed multi-ply fibrous structures are provided.

Method for making multi-ply fibrous structures

Embossed multi-ply fibrous structures and methods for making such embossed multi-ply fibrous structures are provided.

Method of manufacturing laminated armoring material
09925740 · 2018-03-27 · ·

In laminating resin layers on both surfaces of a metal foil layer by adhering a heat-resistant resin layer to a first surface of the metal foil layer and adhering a heat-sealable resin layer to a second surface thereof, as an adhering method, by employing an adhesive agent unapplied portion forming and adhering process in which the resin layer and the metal foil layer are adhered together by applying an adhesive agent to a region of a joining face of both the layers excluding a part of the region so that an adhesive agent unapplied section is formed, a laminated body having the adhesive agent unapplied section is manufactured. A resin layer removal process for removing a resin layer corresponding to the adhesive agent unapplied section of the laminated body to expose the metal foil layer is performed.

ARRAY SUBSTRATE AND MANUFACTURING METHOD THEREOF, POLARIZER ATTACHING FILM AND MANUFACTURING METHOD THEREOF
20180059476 · 2018-03-01 ·

The present invention discloses an array substrate and a manufacturing method thereof, a polarizer attaching film and a manufacturing method thereof. The manufacturing method of an array substrate includes: removing a part of a release film corresponding to a first attaching area of a polarizer, and attaching the first attaching area of the polarizer onto a base substrate such that the first attaching area is in a non-bonding area; and removing a part of the release film corresponding to a second attaching area of the polarizer, and attaching the second attaching area of the polarizer onto the base substrate such that the second attaching area at least partially overlaps with a bonding area.

Window panel for an airframe and method of producing same

The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core.