B29C70/68

Method for producing a body protection item and resulting body protection item
12365151 · 2025-07-22 ·

Manufacturing method of a body protection and resulting body protection, wherein the method comprises producing a structural shell (10) with a maximum thickness of 5 mm, made of thermoplastic material, and defining a concave interior (11) and a convex exterior (12); over-moulding an expanded polystyrene layer (20) overlapping the concave interior (11) of the structural shell (10), producing its adhesion by close contact to the structural shell (10); and wherein the structural shell (10) is produced by means of the distributed placement, in a mould, of a mixture of thermoplastic material and of reinforcing fibres stable at temperatures equal to or lower than the melting temperature of the thermoplastic material, the closure and heating of the mould causing the melting of the thermoplastic material without damaging the reinforcing fibres, and the subsequent cooling of the mould, hardening the thermoplastic material with the reinforcing fibres embedded therein.

Preform charges and fixtures therefor

A preform charge is formed by forming an assemblage of preforms, wherein preforms in the assemblage are bonded to a neighboring preform such that the preform charge effectively becomes a single unit. The preform charge can then be added to a mold to fabricate a part via compression molding.

Preform charges and fixtures therefor

A preform charge is formed by forming an assemblage of preforms, wherein preforms in the assemblage are bonded to a neighboring preform such that the preform charge effectively becomes a single unit. The preform charge can then be added to a mold to fabricate a part via compression molding.

Functional integration of transition structures into fiber reinforced composite layups
12358242 · 2025-07-15 · ·

A method for preparing a multi-material component including providing a fiber reinforced component, the fiber reinforced component having one or more working layers of a fiber reinforced composite material, wherein each of the one or more working layers includes one or more fiber reinforced composite material laminae. The method includes attaching the fiber reinforced component to a multi-material transition component, wherein the multi-material transition component includes a metallic component and a transition laminate includes a transition material, wherein the transition laminate includes one or more partially embedded transition laminae each having a first embedded end that is embedded in the metallic component. Also provided are multi-material transition components and multi-material components provided by the method.

Functional integration of transition structures into fiber reinforced composite layups
12358242 · 2025-07-15 · ·

A method for preparing a multi-material component including providing a fiber reinforced component, the fiber reinforced component having one or more working layers of a fiber reinforced composite material, wherein each of the one or more working layers includes one or more fiber reinforced composite material laminae. The method includes attaching the fiber reinforced component to a multi-material transition component, wherein the multi-material transition component includes a metallic component and a transition laminate includes a transition material, wherein the transition laminate includes one or more partially embedded transition laminae each having a first embedded end that is embedded in the metallic component. Also provided are multi-material transition components and multi-material components provided by the method.

Composite sabot comprising angled undulated fibers, system, and methods of making and using the same
12359900 · 2025-07-15 · ·

A sabot petal is described herein comprising a plurality of woven axial and undulated fibers angled to transfer setback loads. In some cases, the petal is a one-piece component configured to be positioned around a long rod projectile or other aerostructures or aeroshell shapes to be launched with in a gun bore, or rocket or missile launch tube. Corresponding systems and methods are also disclosed.

FIBER-REINFORCED RESIN MOLDED BODY AND METHOD FOR PRODUCING SAME

Provided is a fiber-reinforced resin molded body that has continuous voids and includes a carbon fiber nonwoven fabric and a thermosetting resin, in which the continuous voids have a porosity of 50% by volume to 97% by volume, and contact points of discontinuous carbon fibers constituting the carbon fiber nonwoven fabric are immobilized by the thermosetting resin having a substantially spherical shape of 40 m to 300 m in diameter. Also provided is a method of producing a fiber-reinforced resin molded body, the method including the following steps in the order mentioned: the preform forming step of forming a preform including a carbon fiber nonwoven fabric in a molding die; the injection preparation step of forming a closed space in which the preform is arranged; the injection step of injecting a liquid thermosetting resin into the closed space; the porosity adjustment step of allowing the carbon fiber nonwoven fabric to expand in the thickness direction; and the curing step of maintaining the preform at a temperature equal to or higher than a curing temperature of the thermosetting resin. According to this method, a fiber-reinforced resin molded body that includes a carbon fiber nonwoven fabric and a thermosetting resin is simply produced.

3D over-printing device and method
12384104 · 2025-08-12 · ·

Proposed is a 3D over-printing device for over-printing a 3D shape on an existing structure, the device including: a vat containing a light-curable material; a driving part configured to fix the existing structure and move the existing structure vertically, layer by layer, within the vat; and an optical part comprising a projector and a mirror structure, and configured to photocure an area to be cured on a surface of the light-curable material by projecting UV light in several directions simultaneously from above the surface of the light-curable material toward the surface of the light-curable material that is upward exposed and in contact with the existing structure.

Composite neural conduit
12383272 · 2025-08-12 · ·

A composite nerve conduit comprising an elongated body comprising one or more hollow elongated internal channels for guiding and promoting nerve regeneration. The conduit is a three-dimensional scaffold comprising a crosslinked hybrid/composite matrix of collagen and soy protein isolate having improved mechanical and biocompatibility properties. Methods of using the conduit for promoting nerve regeneration at a site of neural tissue damage by bridging wounded, severed, or damaged nerve sections in a peripheral and/or central nervous system. Methods of fabricating composite neural conduits are also disclosed.

Composite neural conduit
12383272 · 2025-08-12 · ·

A composite nerve conduit comprising an elongated body comprising one or more hollow elongated internal channels for guiding and promoting nerve regeneration. The conduit is a three-dimensional scaffold comprising a crosslinked hybrid/composite matrix of collagen and soy protein isolate having improved mechanical and biocompatibility properties. Methods of using the conduit for promoting nerve regeneration at a site of neural tissue damage by bridging wounded, severed, or damaged nerve sections in a peripheral and/or central nervous system. Methods of fabricating composite neural conduits are also disclosed.