A nozzle for forming a container preform into a plastic container includes a nozzle body and a sealing portion proximate an end of the nozzle body. The sealing portion is configured to engage with a stepped interior of a finish portion of a preform having a longitudinal axis to seal without the use of an O-ring and to preclude any portion of the nozzle body from contacting the sealing surface.

A method for manufacturing a pressure container includes thermally curing a thermosetting resin with which a fiber-reinforced base material is impregnated. The thermally curing step includes thermally curing the thermosetting resin by heat exchange with a fluid supplied to an inside of a liner; and thermally curing the thermosetting resin by heating from an outer surface side of the fiber-reinforced base material. A temperature of the fluid supplied to the inside of the liner is higher than a temperature of the helating from the outer surface side of the fiber-reinforced base material so that the thermosetting resin is thermally cured from an inner surface side of the fiber-reinforced base material adjacent to the liner before the outer surface side of the fiber-reinforced base material.

A foam molded article includes a main agent resin, a filler of greater than or equal to 15% by mass and less than or equal to 80% by mass, and a foaming agent of greater than or equal to 0.01% by mass and less than or equal to 10% by mass, and a foaming ratio caused by the foaming agent is greater than or equal to 1.1 times.

A method for producing an orthodontic or dental appliance includes laminating a layer of polyethylene terephthalate (PET) with a layer of polyethylene to form a multilayer film, forming the multilayer film into the shape of an orthodontic appliance, trimming the formed film to a desired shape, and removing the layer of polyethylene. In one embodiment, the appliance is a multi-layer structure formed from two adjacent layers of PET with a plurality of functional elements such as sensors or actuators between the two layers.

The present invention provides a method for manufacturing a press-molded body, the method having a step for disposing an X material inside a mold, a step for closing the mold and extruding a Y material, which is a kneaded material, into the mold after pressure has begun to be applied to part of the X material, and a step for cold-pressing and integrally molding the X material and the Y material inside the mold, wherein: the X material includes reinforcing fibers FA, having a weight-average fiber length Lw.sub.A, and a thermoplastic resin R.sub.X; the Y material includes reinforcing fibers FB, having a weight-average fiber length Lw.sub.B, and a thermoplastic resin R.sub.Y; Lw.sub.B<Lw.sub.A; Lw.sub.A is 1 mm or greater and 100 mm or less; the X material has a spring-back amount greater than 1.0 and less than 14.0; the press-molded body has an vertical plane part and a top plane part; during the cold pressing, the Y material is caused to move from a region other than a vertical plane portion to the vertical plane portion; and a thickness t1 of the vertical plane portion and a thickness t2 of the top plane portion satisfy t1>t2.

Disclosed is a bionic fiber-reinforced composite material with high impact resistance and a preparation method thereof. Bionic fiber composite material is composed of positive and negative spiral fiber resin layers, which are alternately laid in a particular proportion and then heated and cured under pressure. The positive and negative spiral fiber resin layers are non-coaxial and uniformly rotated and stacked along their respective central axes periodically. The bionic fiber resin layer is formed by infiltrating a structurally bionic fiber material with a modified resin. The bionic structures include a scorpion claw structure, a jaw foot structure of mantis shrimp and a combined structure in the horn sheath of small tail Han sheep and pheasant feathers. Significantly, bionic fiber-reinforced composite material effectively improves the impact resistance and interlayer toughness of the fiber composite material by undergoing the combinatorial bionics of the structure of fiber material and the layering method.

A composite material forming device forms a composite material including a resin and reinforced fibers having electrical conductivity. The composite material forming device includes: a conduction jig having electrical conductivity, the conduction jig being to be placed on a surface of the composite material so as to make a bridge between both end portions of the reinforced fibers in a fiber direction; and an electric current generating unit that generates an electric current in the conduction jig. The conduction jig placed on the surface of the composite material and the reinforced fibers form a closed loop through which the electric current flows so that the closed loop intersects the surface of the composite material.

A foam molded article includes a main agent resin, a filler of greater than or equal to 15% by mass and less than or equal to 80% by mass, and a foaming agent of greater than or equal to 0.01% by mass and less than or equal to 10% by mass, and a foaming ratio caused by the foaming agent is greater than or equal to 1.1 times.

Provided is a molding method of a sealing cover, realized by setting up a sealing cover mold, the mold includes a cavity and a core group arranged in the cavity, including setting up a first core and a second core, the mold opening direction of the first core and the second core are not parallel. The present application does not need a process hole to perform the injection molding of the sealing cover with a fastening structure, whose sealing is also better.

A spacer structure for a sandwich construction, formed from a material web which is provided with a plurality of cuts and which has a material web plane as a first plane, wherein, by forming the material web, at least one support platform is formed in portions which is spaced at a distance from the first plane and is arranged in a second plane. Spacing elements run along a direction of extent (Ε) from the first plane into the second plane in the transition zone from the first plane into the second plane and thus the spacing elements space the first plane apart from the support platform, the spacing elements having a twist about the direction of extent thereof along the direction of extent thereof (Ε), the twist being formed by the shaping of the material web being performed as bending.