A damage recovery system of a fuselage of an aircraft, comprising: a tank containing a polyurethane foam; a main duct fluidically coupled to the tank to receive the foam; secondary ducts fluidically coupled to the main duct; and distribution means adapted to allow an outflow of the foam from the secondary ducts. Graphene powder can be mixed and added to the polyurethane foam. In flight, a possible leak (crack or hole) in the fuselage is plugged by the polyurethane foam with graphene powder.

The present invention provides a metal pipe coated on at least a section of the metal pipe with a polyolefin coating system, wherein the system consists of the following layers: (a) optionally, a corrosion protective layer of a chromate, phosphate or other salt; (b) a polyolefin based adhesive, preferably in a thickness of 0.3-5 mm; (c) a PE or PP coating layer, preferably in a thickness of 1-10 mm; (d) optionally, an adhesion promoting layer between the polyolefin based adhesive and a PE or PP layer; wherein the polyolefin based adhesive contains an organic phase consisting of substantially saturated hydrocarbons, and wherein the adhesive contains amorphous polypropylene, ethylene-propylene copolymers or poly(iso)butylene (co)polymers, said adhesive being flowable when a pressure of 10 kgf/cm.sup.2 is applied, wherein the PE or PP coating is a continuous layer over the coated section, and wherein said polyolefin based adhesive adheres to both the metal pipe and to said PE or PP coating.

A diffusion barrier structure, and a conductive laminate and a manufacturing method thereof are provided. The conductive laminate includes a substrate, a diffusion barrier structure, and a conductive layer. The diffusion barrier structure is formed between the substrate and the conductive layer. The diffusion barrier structure includes a discontinuous modifying layer and a barrier layer. The discontinuous modifying layer is disposed on the substrate. A material for composing the discontinuous modifying layer is a polymer with hydrophilic group. The barrier layer is disposed on the substrate and the discontinuous modifying layer. A material for composing the barrier layer includes at least one self-healing polymer.

A fuel cell containing fuel for an aircraft includes an innermost layer configured to contact the fuel, an outermost layer and a containment gel formed from isocyanate and polyol interposed between the innermost and outermost layers. The containment gel is configured to self-seal a ballistically formed hole therein, thereby reducing leakage of the fuel from the fuel cell.

The present invention relates to a protective film for a windshield of a vehicle, which can be installed on a curved portion of the windshield of the vehicle without a thermoforming process, thereby improving the workability of a worker, and improving impact resistance to effectively protect the windshield of the vehicle.

A method for manufacturing a conductive laminate and a conductive laminate are provided. The method for manufacturing the conductive laminate includes steps of: providing a substrate having a surface; immersing the substrate into a modifying solution including a silane with a hydrophilic group to form a discontinuous modified layer on the surface of the substrate; forming a barrier layer on the surface of the substrate and the discontinuous modified layer, and forming a conductive layer on a surface of the barrier layer. The barrier layer includes a polymer, and the polymer is selected from the group consisting of: polyvinyl alcohol, polyvinylpyrrolidone, polyacrylic acid, polyethylene glycol, and any combination thereof.

An article includes a hybrid nanocomposite product, which includes a nanostructure array and a resin matrix contained among and/or around the nanostructure array. The array/matrix is placed in between layers of dry or resin-infused fiber composite to permit formation of a composite structure. The nanostructure array and/or the resin matrix may be disposed in an abutting relationship with other layers of a composite. The array/matrix can provide reinforcement of the composite in the z-direction. Transfer of resin into dry fiber forms may be provided when the array/matrix acts as a resin transfer medium. Nanostructure arrays with a resin matrix can be prepared to form a resin film product. Methods are presented for infusing composites via resin-transfer molding (RTM), vacuum-assisted resin transfer molding (VARTM), resin film infusion (RFI), or injection molding wherein a resin matrix film substantially maintains alignment and position of the nanostructure array during the infusion process.

Provided are cementitious panel that include a swellable material within a core layer, a dense layer, and/or a sheet of facing material that make up a cementitious panel, as well as methods of manufacturing such cementitious panels that include a swellable material and methods of providing a moisture or water barrier in a cementitious panel.

Provided herein are a fabric-based substrate and an organic electronic device including the same. The fabric-based substrate includes a fabric layer having an upper surface and a lower surface. A plurality of electrodes are disposed on the upper surface of the fabric layer. An adhesive layer is provided on the upper surface and the lower surface of the fabric layer and filled at least some empty regions between the electrodes and the fabric layer, between the electrodes, and at least some pores in the fabric layer. A self-healing polymer layer is disposed on the adhesive layer located on the lower surface of the fabric layer.

A method for manufacturing a conductive laminate and a conductive laminate are provided. The method for manufacturing the conductive laminate includes steps of: providing a substrate having a surface; immersing the substrate into a modifying solution including a silane with a hydrophilic group to form a discontinuous modified layer on the surface of the substrate; forming a barrier layer on the surface of the substrate and the discontinuous modified layer, and forming a conductive layer on a surface of the barrier layer. The barrier layer includes a polymer, and the polymer is selected from the group consisting of: polyvinyl alcohol, polyvinylpyrrolidone, polyacrylic acid, polyethylene glycol, and any combination thereof.