A fiber-reinforced fabric, composite materials formed from such fabrics, and methods of making the fiber-reinforced fabric or composite materials, are provided. The fabrics and composite materials demonstrate improved fatigue performance relative to conventional fiber-reinforced fabrics.

Gypsum panels and methods for their manufacture are provided herein. The gypsum panels include a gypsum core having a first surface and a second opposed surface and a first fiberglass mat associated with the first surface of the gypsum core, such that gypsum from the gypsum core penetrates at least a portion of the first fiberglass mat.

Gypsum panels and methods for their manufacture are provided herein. The gypsum panels include a gypsum core having a first surface and a second opposed surface and a first fiberglass mat associated with the first surface of the gypsum core, such that gypsum from the gypsum core penetrates at least a portion of the first fiberglass mat.

In a method of manufacturing a semiconductor device, a mask layer and a first layer may be sequentially formed on a substrate. The first layer may be patterned by a photolithography process to form a first pattern. A silicon oxide layer may be formed on the first pattern. A coating pattern including silicon may be formed on the silicon oxide layer. The mask layer may be etched using a second pattern as an etching mask to form a mask pattern, and the second pattern may includes the first pattern, the silicon oxide layer and the coating pattern. The mask pattern may have a uniform size.

An etching method includes etching a silicon substrate with a liquid composition containing an alkaline organic compound, water, and a boron compound with a content in the range of 1% by mass to 14% by mass. The boron compound is at least one of boron sesquioxide, sodium tetraborate, metaboric acid, sodium perborate, sodium borohydride, zinc borate, and ammonium borate.

One illustrative method disclosed herein includes, among other things, forming a fin-removal masking layer comprised of a plurality of line-type features, each of which is positioned above one of the fins, and a masking material positioned at least between adjacent features of the fin-removal masking layer and above portions of an insulating material in the trenches between the fins. The method also includes performing an anisotropic etching process through the fin-removal masking layer to remove the portions of the fins to be removed.

A support structure includes an internal cavity. An elastic membrane extends to divide the internal cavity into a first chamber and a second chamber. The elastic membrane includes a nanometric-sized pin hole extending there through to interconnect the first chamber to the second chamber. The elastic membrane is formed of a first electrode film and a second electrode film separated by a piezo insulating film. Electrical connection leads are provided to support application of a bias current to the first and second electrode films of the elastic membrane. In response to an applied bias current, the elastic membrane deforms by bending in a direction towards one of the first and second chambers so as to produce an increase in a diameter of the pin hole.

A lighted assembly includes a perforated member having a plurality of relatively small openings therethrough. The openings are arranged to provide areas forming letters, designs, or the like. A light source may be positioned adjacent the perforated member whereby light from the light source travels through the openings to form illuminated letters, designs or the like. The perforations may be filled with a light-transmitting polymer material. The light source may comprise an LED and a light guide that distributes light along a lower side of the perforated member. The light source may be positioned in a waterproof housing that is sealed to the perforated member.

A method for forming a plurality of precision holes in a substrate by drilling, including affixing a sacrificial cover layer to a surface of the substrate, positioning a laser beam in a predetermined location relative to the substrate and corresponding to a desired location of one of the plurality of precision holes, forming a through hole in the sacrificial cover layer by repeatedly pulsing a laser beam at the predetermined location, and pulsing the laser beam into the through hole formed in the sacrificial cover layer. A work piece having precision holes including a substrate having the precision holes formed therein, wherein a longitudinal axis of each precision hole extends in a thickness direction of the substrate, and a sacrificial cover layer detachably affixed to a surface of the substrate, such that the sacrificial cover layer reduces irregularities of the precision holes.

Provided is a method for manufacturing an aerogel blanket having improved processability by reducing manufacturing time and cost, the method including the steps of mixing a precursor material, an acid catalyst and a hydrous alcohol to prepare a sol, depositing a substrate in the sol, and reacting with a gaseous silazane-based compound to form a gel and to perform aging and surface modification reaction simultaneously to form a wet gel blanket, and drying the wet gel blanket to manufacture an aerogel blanket.