Patent classifications
B32B2262/14
FLAME RESISTANT MATERIAL FOR A PROTECTIVE GARMENT
Oxidized polyacrylonitrile fiber (OPF) containing fabrics when used in the fire service, either in a NFPA 1971 or NFPA 1951 compliant protective garments, offer exceptional comfort and protection characteristics that ensure firefighters can safely perform their duties in structural fire, overhaul, urban search and rescue, and other various missions. OPF containing fabrics used in turnout gear outer shells and compliant with NFPA 1971, provide the best combination of protection as tested by the thermal protective performance test and comfort as tested by the total heat loss/resistance to evaporative heat transfer test.
Multilayer structure for transporting heat transfer fluid
A tubular structure for transporting heat transfer fluid including at least: i) a layer (1) in contact with the fluid including at least one thermoplastic polymer P1 that is semicrystalline with Tm1 greater than or equal to 160° C., as determined according to the standard 1 1357-3 (2013) or amorphous with Tg1 greater than or equal to 100° C., as determined according to the standard 1 1357-2 (2013), said layer (1) containing no fibers, ii) a layer (2) including at least: (a) a thermoplastic polymer P2 that is semicrystalline, in particular a polyamide with Tm2 greater than or equal to 170° C. or amorphous with Tg2 greater than or equal to 100° C., or a polyolefin with Tm greater than 100° C.; (b) optional continuous fibers, the polymer P2 being identical to P1 or different from P1 in which case the polymers P1 and P2 adhere at least partially to one another.
Multilayer substrate materials for application to textile fabrics
A multilayer substrate material configured to be applied to a back surface of an upholstery or mattress textile fabric and a front surface configured to contact a user of the upholstery or mattress textile fabric. The multilayer substrate material includes protector, adhesive, film and backcoat layers. The adhesive layer is applied to the protector layer and formed of a number of discrete and non-continuous regions. The film layer is applied to the adhesive layer. The number of discrete and non-continuous regions include an interface between the protector layer and the film layer such that the protector layer touches the film layer at the interface. The backcoat layer is applied to the film layer and includes a non-acrylic binder and a flame retardant material. The number of discrete and non-continuous regions form a number of non-adhesive regions therebetween configured to not resist flexing of the protector, film and backcoat layers.
Apparel with body mapped waterproof-breathable portions
A garment includes a first material layer including a first surface, a second material layer laminated to the first material layer, where the second material layer includes a second surface, and a laminate material disposed in a non-continuous manner between the first and second surfaces of the first and second material layers. An amount of laminate material disposed between the first and second material layers varies at different zones defined along the first surface of the first material layer. The laminate material can be applied via a dot lamination process so as to form an array of laminate dots that varies by one or more of spacing between laminate dots, dimensions of laminate dots and shapes of laminate dots at the different zones.
Self-healing interlaminar delamination in fiber-reinforced composites via thermal remending
Disclosed herein is an intrinsically self-healing composite based upon in situ thermal remendability of an embedded polymeric interphase. The fiber-reinforced composite (FRC) material may incorporate a thermoset polymer with a defined glass transition temperature (T.sub.g) and/or a thermoplastic material of amorphous or semi-crystalline nature. The polymeric interphase can be incorporated as a plurality of particles, fibers, meshes, films, or 3D-printed structures. The self-healing composite includes a resistive heating component as a structural element that minimizes electrical energy demand and impact on mechanical integrity. Healing occurs in situ via resistive heating and can be enabled below, at, or above the glass-transition temperature of the FRC matrix, demonstrating viability for in-service repair under sustained loads. In addition to providing rapid healing functionality, the polymeric interphase increases inherent resistance to interlaminar fracture. Repeated heal cycles have been achieved in a double cantilever beam (DCB) fracture test without significant degradation in performance.
Curative
An illustrative embodiment of a manufactured surface component may be comprised of a textile material on a first face and an elastomer material on a second face, wherein said elastomer material is bonded to said textile material, wherein said manufactured surface component is substantially planarly configured, wherein an area of said first face and said second face is from about 0.04 square inches to about 4.0 square inches, wherein a thickness of said manufactured surface component is from about 0.3 mm to about 2.5 mm, and wherein said manufactured surface component is substantially free of any petrochemical-derived plastics, petrochemicals, and toxins.
COMPOSITE ARTICLES PROVIDING FLAME RETARDANCY AND NOISE REDUCTION
A thermoplastic composite article comprising a porous core layer and an open cell skin disposed on a first surface of the core layer is described. The composite article comprises a noise reduction coefficient of at least 0.5 as tested by ASTM C423-17 and a flame spread index of less than 25 and a smoke development index of less than 150 as tested by ASTM E84 dated 2009.
PISTON INCLUDING A COMPOSITE LAYER APPLIED TO METAL SUBSTRATE
A piston for a heavy duty diesel engine including a composite layer forming at least a portion of a combustion surface is provided. The composite layer has a thickness greater than 500 microns and includes a mixture of components typically used to form brake pads, such as a thermoset resin, an insulating component, strengthening fibers, and an impact toughening additive. According to one example, the thermoset resin is a phenolic resin, the insulating component is a ceramic, the strengthening fibers are graphite, and the impact toughening additive is an aramid pulp of fibrillated chopped synthetic fibers. The composite layer also has a thermal conductivity of 0.8 to 5 W/m.Math.K. The body portion of the piston can include an undercut scroll thread to improve mechanical locking of the composite layer. The piston can also include a ceramic insert between the body portion and the composite layer.
Insulating Materials And Methods Thereof
Insulating articles, assemblies and methods are provided. The insulating articles include a core layer (101,201) containing a plurality of non-meltable fibers; and at least one reinforcement layer (102, 202) disposed on the core layer (101,201). The insulating article has tensile strength of at least 0.75 newtons/millimeter according to ASTM D822 and a tear strength of at least 2 newtons under ASTM D1938, wherein the insulating article has a surface electrical resistivity of at least 15 M-ohm at a relative humidity of 85% and temperature of 30° C., wherein the insulating article has an air flow resistance of up to 2000 MKS Rayls according to ASTM C522, and wherein the insulating article displays a UL94-V0 flammability rating.
LAYERED BODY
It is provided that a layered body having excellent absorption speeds of fuel and the like to the filter media. A layered body comprising a first base material and a second base material, wherein the first base material and the second base material are adhered to each other via an adhesive, the first and second base materials each contain a phenol-based resin and an aliphatic hydrocarbon detected during a retention time of 12.0 to 30.0 minutes under pyrolysis-gas chromatography mass spectrometry (PY-GC/MS), and the adhesive contains 65 mol % or more of a butylene terephthalate unit and 5 mol % or more of a butylene isophthalate unit, and has an acid value of not larger than 100 eq/ton, a glass transition temperature of −10 to 60° C., and a specific gravity of not less than 1.20.