B32B2307/708

Square symmetric double-double laminate structures and methods for manufacturing and using the same

Square symmetric composite laminate structures, and sub-modules thereof, are provided, along with methods of forming the same. The square symmetric laminate structures include two or more sub-laminate modules, each comprising: a first ply set consisting of a first ply layer oriented at a first angle and a second ply layer oriented at a second angle, a first sum of the first and second angles being ninety degrees; and a second ply set consisting of a third ply layer oriented at a third angle and a fourth ply layer oriented at a fourth angle, a second sum of the third and fourth angles being ninety degrees; wherein the second ply layer is positioned adjacent the third ply layer and the second and third ply layers are both positioned intermediate the first and fourth ply layers, thereby defining a double-double helix arrangement of the respective ply layers. Associated methods are also provided.

VISIBLY TRANSPARENT BROADBAND INFRARED MIRROR FILMS

Multilayer infrared (IR) reflecting films are provided. An optical repeating unit of the film include a plurality of optical polymeric layers arranged to reflect light by constructive and destructive interference. Optical layer A is a high refractive index polymeric layer, and optical layer B is a low refractive index isotropic polymeric layer containing fluoropolymers. The film has an average reflectance of about 50% to about 100% in a near infrared wavelength range of about 850 nm to about 1850 nm, and an average transmission of about 70% to about 90% in a visible light range.

Method for producing fiber-reinforced plastic

Provided are methods for producing a fiber-reinforced plastic having high mechanical properties and high productivity during molding of a complicated shape. In one aspect, the method produces a fiber-reinforced plastic using a tape substrate A and a sheet substrate B, the tape substrate A being a tape-shaped substrate including one or more sheets of incised prepreg a; the incised prepreg a being a prepreg including unidirectionally oriented reinforcing fibers and a resin and having a plurality of incisions dividing the reinforcing fibers formed in the prepreg, and satisfying the following condition 1; the sheet substrate B being a substrate including randomly oriented reinforcing fibers and a resin. In another aspect, the method for producing a fiber-reinforced plastic includes: a placement step \ (A) of placing a plurality of tape substrates A on a mold such that each of the sheet substrates A forms an overlapping portion in which the sheet substrate A overlaps one or more other sheet substrates A and a non-overlapping portion in which the sheet substrate A does not overlap any other sheet substrates A, a placement step (B) of placing a sheet substrate B, and a molding step of heating and pressing the tape substrates A and the sheet substrate B placed. Condition 1 is: the average length xa of the incisions and the average length ya of the reinforcing fibers divided by the incisions satisfy ya>6.0xa+10.

System, method, and apparatus for magnetic surface coverings

The present invention pertains to the art of floor coverings, and, more particularly to an apparatus for use in securing floor covering units to an underlay and a method of manufacturing said floor covering units and said underlay. More particularly, the present invention relates to an apparatus, method, and method of manufacturing magnetized floor covering units and magnetized underlays for securing magnetized floor covering units.

AUTOMATED PLACEMENT OF COMPOSITE MATERIAL

Methods and systems for automated placement of composite material on a surface of a component, the composite material including unidirectional fibers, is provided. A set of fiber paths along the surface is established, the set of fiber paths comprising at least one ply, each ply comprising a respective plurality of fiber paths being substantially aligned with a respective direction. An isotropy factor for the component is determined based on the set of fiber paths, the isotropy factor being indicative of a distribution of the plurality of fiber paths on the surface. When the isotropy factor exceeds a predetermined threshold, a respective layer of composite material is applied to the surface of the component using an automated fiber placement machine and for each of the at least one ply, wherein the unidirectional fibers of the composite material are applied along the set of fiber paths.

Densified foam for thermal insulation in electronic devices

A heat spreading and insulating material using densified foam is provided that has a heat spreading layer that is adhered to an insulating layer. The material is designed to be used with mobile devices that generate heat adjacent to heat sensitive components. The insulating layer is formed from a compressed layer of polyimide foam to increase its density. The polyimide foam retains a significant amount of insulating properties through the densification process. In some embodiments, an EMI shielding layer is added to improve electrical properties of the device. The heat spreading layer is commonly a graphite material with anisotropic heat properties that preferentially conduct heat in-plane. The material may also include pressure sensitive layers to permanently apply the material to the mobile device.

REFLECTIVE FILM ASSEMBLED ON A COMPOSITE STRUCTURE
20190308752 · 2019-10-10 · ·

A space vehicle including a reflective component on the side thereof for reflecting electromagnetic radiation, such as a mirror, the composite being formed by the steps of providing a composite support structure; providing a release liner including a metallic layer having a thickness between 1 and 5 microns on a surface thereof; situating the release liner against the surface of the composite support structure so that the metallic layer of the release liner is placed in direct, physical contact with the surface of the support structure; removing the release liner so that the metallic layer remains attached to the surface of the support structure; and mounting the support structure on a support on the exterior of the space vehicle.

TOUCH PANEL AND MANUFACTURING METHOD THEREOF
20190302913 · 2019-10-03 ·

A touch panel is provided. The touch panel includes a substrate, a ground layer, a passivation layer, a conductive layer and a shielding layer. The ground layer is disposed on and covers a portion of a surface of the substrate. The passivation layer is disposed on the ground layer, thereby the ground layer has a covered portion and an exposed portion. The covered portion is covered by the passivation layer. The conductive layer is disposed on and completely covers the exposed portion of the ground layer. A portion of the passivation layer is covered by the conductive layer. The shielding layer is disposed on the conductive layer, and the orthogonal projections of the shielding layer and the ground layer onto the surface of the substrate are at least partially overlapped with each other. The present invention also provides a manufacturing method of a touch panel.

Composite epoxy material with embedded silicon carbide and alumina nanoparticles

A stacked composite material and a method of preparation, wherein the stacked composite materials comprises of glass fiber layers sandwiched between nanocomposite layers. The nanocomposite layers comprise a nanofiller dispersed in a cured epoxy matrix, wherein the nanofiller is at least one of silicon carbide nanoparticles or aluminum oxide nanoparticles. Adjacent and noncontiguous glass fiber layers are oriented in a unidirectional orientation or a quasi-isotropic orientation.

Thermally insulating sheet formed from a down core structure and method of fabrication
20190283078 · 2019-09-19 ·

A thermally insulating sheet formed by a down core structure which is comprised solely of down feather material mixed with binding material which is heat fused together to form a homogeneous sheet core. The method of fabricating the homogeneous thermally insulating sheet to form the down core structure is described. This novel method restrains the down clusters and binding material during the process of mixing, depositing, conveying and heat fusing to form a homogeneous down core sheet. The down core structure is subjected to two separate heat treatments which produces a down core sheet having at least some of its outer surfaces being of higher bond density than the inside of the core.