Patent classifications
B32B5/266
ACOUSTIC INSULATION MATERIAL
An acoustic insulation web of fibrous material includes: a nonwoven batting including: a first layer including a first plurality of low-melt binder fibers forming a first predetermined percentage of the first layer; and a second layer bonded with the first layer and including a second plurality of low-melt binder fibers forming a second predetermined percentage of the second layer, the first predetermined percentage being greater than the second predetermined percentage such that the first layer is denser than the second layer.
Multilayered nonwoven fabric containing submicron fibers, a method of manufacture, an apparatus, and articles made from multilayered nonwoven fabrics
This document presents a novel method of manufacturing multilayered nonwoven fabrics consisting of submicron fibers, hydroentangled, meltfibrillated, and/or spunlaid web layers. The composite multilayered webs contain one or more submicron fiber webs placed between inner and outer layers of hydroentangled, meltfibrillated, and/or spunlaid web, forming a fabric that may be utilized in the manufacture of articles which serve as barriers, wipes or sorbent materials, or may have other potential applications. The created novel composite multilayered fabric may have increased loft, softness and bending length, may not be solely dependent upon an electrostatic charge to repel small particles and microbes, and may be formed from a broad selection of natural, synthetic, and recycled polymers, including petroleum- and plant-based, allowing polymer selection based on article lifecycle.
PROTECTIVE COMPOSITE FABRICS AND METHODS OF MANUFACTURE AND USE
A composite fabric includes a film, a first fibrous layer, a fabric layer, and a second fibrous layer. The film has a first side and a second side. The first fibrous layer has a first side connected to the second side of the film and a second side. The fabric layer has a first side connected to the second side of the first fibrous layer and a second side. The second fibrous layer has a first side connected to the second side of the fabric layer and a second side. The film can be a non-heat shrinking film. The composite fabric may also include one or more retaining members for contacting a surface on which the composite fabric is placed and resisting movement of the composite fabric relative to the surface.
MOLDED CEILING MATERIAL FOR VEHICLE AND PRODUCTION METHOD THEREFOR
A ceiling material body (1a) includes a substrate layer (2) formed from rigid urethane foam; a first fiber-reinforced layer (3) provided on an in-cabin side of the substrate layer (2); a second fiber-reinforced layer (4) provided on an out-cabin side of the substrate layer (2); a surface layer (5) provided on an in-cabin side of the first fiber-reinforced layer (3); and a back layer (6) provided on an out-cabin side of the second fiber-reinforced layer (4). The second fiber-reinforced layer (4) includes a glass paper (7) overlaying the substrate layer (2) and a glass mat (8) overlaying an opposite side of the glass paper (7) from the substrate layer (2).
COMPOSITE TYPE HEAT INSULATOR AND METHOD FOR PRODUCING THE SAME
Provided are a composite type heat insulator having an excellent heat insulating properties at high temperatures regardless of its thin body, and a method for producing the same. The composite type heat insulator comprises a first and a second cloths composed of silica fibers having a hydroxyl group; and a heat insulating layer sandwiched between the first and the second cloths. The heat insulating layer contains a silica aerogel and silica staple fibers having a fiber length of 0.5 to 5 mm. The heat insulating layer may optionally contain an infrared absorber and/or a film-forming inorganic binder.
Acquisition Distribution Layer
Acquisition-distribution-layers (ADL) comprising a hydroentangled composite are provided. The hydroentangled composite includes (a) a first outer layer including a first plurality of synthetic fibers, (b) a second outer layer including a second plurality of synthetic fibers, and (c) at least one core layer including cellulose fibers comprising natural cellulose fibers, synthetic cellulose fibers, or a combination thereof, in which the at least one core layer is located directly or indirectly between the first outer layer and the second outer layer. The first plurality of synthetic fibers, the second plurality of synthetic fibers, and the cellulose fibers are physically entangled together. The hydroentangled composite further comprises a three-dimensional topography defined by a first outermost surface of the hydroentangled composite, in which the three-dimensional topography includes a plurality raised portions and a plurality of recessed portions.
Fiberglass Veils Containing Fire-Retardant Minerals and Refractive Particles, and High Gloss and/or Fire-Retardant and/or Non-Combustible Laminates Containing Such Veils
Non-woven fiberglass veils, and laminates made therefrom, comprising: a plurality of glass fibers; a resin component; a fire-retardant component; and a particulate component, the particulate component comprising inorganic particles having a refractive index higher than a refractive index of the fire-retardant component and an average particle size of from about 0.1 to about 0.5 μm; wherein the fire-retardant component and the particulate component are present in a combined amount of from about 50% to about 90% by weight, based on the total weight of the veil, and wherein the fire-retardant component and the particulate component are present in a ratio by weight of from about 95:5 to about 50:50; are described.
High Temperature Flexible Insulation For Extreme Environments
A flexible insulation material may be configured to substantially reduce the amount of radiation transmitted therethrough by incorporating a reflective mat of high temperature fibers that withstand temperatures of at least 500° C. The flexible insulation may be stored and used over temperatures ranging from −270° C. to 5000° C. The mat may have optical properties to produce a transmittance of no more than 5% over a range of temperature from 500° C. to 5000 vC. The mat may include high temperature fibers such as carbon and/or silicon carbide and these fibers may be coupled by a binder in a non-woven fabric. The flexible insulation material may be configured in the Flexible Thermal Protection System of a deployable aerodynamic decelerator or a Hypersonic Inflatable Aerodynamic Decelerator and may be durably flexible.
Laminated nonwoven fabric
The present invention provides a laminated nonwoven fabric achieving both handling properties during manufacturing and use and adherence to a skin surface at a high level particularly when used for a face mask. The laminated nonwoven fabric includes a nonwoven fabric layer (A) and a nonwoven fabric layer (B). The nonwoven fabric layer (A) is formed from a fiber A having a single fiber diameter of 50 nm or more and 800 nm or less, and the nonwoven fabric layer (B) is formed from a fiber B having a single fiber diameter of 3 μm or more and 30 μm or less. The nonwoven fabric layer (B) includes 15 to 40% by mass of a fiber B1 to all of the fibers constituting the nonwoven fabric layer (B), the fiber having tensile strength of 2.0 cN/dtex or less as measured based on JIS L 1015: 2010 8.7.2. The nonwoven fabric layer (B) Includes a fiber B2 having tensile strength exceeding 2.0 cN/dtex as measured based on JIS L 1015: 2010 8.7.2. The nonwoven fabric layer (A) is disposed as an outermost layer of at least one surface.
SCREW FEEDER AND FIBER STRUCTURE MANUFACTURING APPARATUS
A screw feeder includes: a case that includes a material putting-in portion through which a fluff material is put in and a material putting-out portion through which the fluff material is put out below the material putting-in portion; and a screw that includes a rotational shaft and a blade portion, the rotational shaft being provided rotatably inside the case, the blade portion being spirally mounted on the rotational shaft; wherein the screw is rotated with repeated alternation of a slope-down direction in which the blade portion slopes downward spirally in a vertical direction and a slope-up direction in which the blade portion slopes upward spirally in the vertical direction.