Resin dissolved or suspended in liquid is applied to a greige fabric formed with finer denier yarns forming surface loops before the fabric is bulked and after the liquid has been removed by low-temperature drying. The dried fabric is then bulked at a higher temperature setting the resin, resulting in superior loop tip resilience, and superior surface durability. Bulking and simultaneous resin setting optionally includes shrinking in area by 10-20%. Print appearance retention is also superior when printing follows bulking and setting of the resin.

Composite materials are provided which may include one or more sheets of carbon fibers woven in orthogonal direction bundles; carbon nanotubes embedded within pores between the bundles; and a matrix material in which the one or more sheets and the carbon nanotubes are embedded. In one case, the carbon fibers lie substantially in an x-direction and a y-direction and the carbon nanotubes are oriented substantially in a z-direction, which is substantially perpendicular to the x- and y-directions. Methods for making the composite materials are also provided.

Provided are a cover window and an apparatus and method for manufacturing the cover window. The cover window includes a film layer having at least one bent portion, a resin layer having at least one bent portion, and an adhesive layer disposed between the film layer and the resin layer and adhering the film layer and the resin layer.

A skin-to-core bond line mapping system and method is disclosed. Layered composite components formed by “sandwiching” multiple materials together require a continuous bond between those materials with voids below particular thresholds that can vary by application. The skin-to-core bond line mapping system can include a laminate, an adhesive, a separator film, a core, a breather, a layup tool, bagging material, sealant, and a vacuum port. By employing systems and processes that layer separator film over adhesive and applying a core proximate the adhesive, a bagging material can be disposed over the materials to facilitate vacuum compaction, thereby impressing core impressions on the adhesive to map the areas between the skin and core that have good contact. An iterative process is disclosed, in which additional adhesive can be used to build the bond line until contact is made (or engineering tolerance is reached).

Resin dissolved or suspended in liquid is applied to a greige fabric formed with finer denier yarns forming surface loops before the fabric is bulked and after the liquid has been removed by low-temperature drying. The dried fabric is then bulked at a higher temperature setting the resin, resulting in superior loop tip resilience, and superior surface durability. Bulking and simultaneous resin setting optionally includes shrinking in area by 10-20%. Print appearance retention is also superior when printing follows bulking and setting of the resin.

Resin compositions, layers, and interlayers comprising a poly(vinyl acetal) resin that includes residues of an aldehyde other than n-butyraldehyde are provided. Such compositions, layers, and interlayers can exhibit enhanced or optimized properties as compared to those formulated with comparable poly(vinyl n-butyral) resins.

The present disclosure provides a bonding device for a flexible panel including: a transport element, a vacuum chamber, a cover jig, and a bonding jig; wherein the transport element is configured to move the flexible panel into the vacuum chamber or move the flexible panel out of the vacuum chamber; wherein both the cover jig and the bonding jig are disposed in the vacuum chamber, the cover jig is opposite to the bonding jig, and the cover jig is configured to secure thereon a cover plate to be bonded; and wherein the bonding jig has a curved hump protruding toward the cover jig, and the hump is configured to raise the flexible plate up to the cover plate to bond the cover plate with the flexible panel when the transport element transports the flexible plate to a location below the cover plate.

This invention provides methods for the processing of platinum metallized high temperature co-fired ceramic (HTCC) components with minimum deleterious reactions between platinum and the glass constituents of the ceramic-glass body. The process comprises co-firing a multilayer laminate green ceramic-glass body with via structures filled with a platinum powder-based material in a reducing atmosphere with a specified level of oxygen partial pressure. The oxygen partial pressure should be maintained above a minimum threshold value for a given temperature level.

In accordance with one embodiment of the present disclosure, a method for manufacturing a honeycomb core sandwich panel includes placing a thermoset facesheet in contact with a thermoplastic honeycomb core without using a separate adhesive and attaching the thermoset facesheet to the thermoplastic honeycomb core by using a curing profile comprising a temperature that is lower than a gel point temperature of the thermoset facesheet and higher than a softening point temperature of the thermoplastic honeycomb core.

A gas barrier film has, in sequence, a support, an inorganic layer, and a resin film, the inorganic layer and the resin film being supported on the support. The resin film has a hydroxy group. The inorganic layer and the resin film are directly joined to each other with separate portions that are partially present at an interface between the inorganic layer and the resin film. The gas barrier film has one or more sets of a combination of the inorganic layer and the resin film. A method for producing the gas barrier film includes forming an inorganic layer by a gas-phase deposition method, subsequently laminating a resin film having a hydroxy group with the inorganic layer, and heating the resulting film laminate.