A method for treating a core material is provided. A method for preparing a composite material, the composite material prepared by the method, and the use thereof is also provided.

The present invention relates to the technical field of composite materials, and in particular to a fiber composite material and a preparation method thereof. The preparation method comprises: A) uniformly dispersing nanoparticles in a solvent to obtain a nanoparticle dispersion; B) uniformly spray-coating the nanoparticle dispersion on a chopped fiber nonwoven fabric, and drying the fabric to obtain a nano-modified chopped fiber nonwoven fabric; C) intercalating the nano-modified chopped fiber nonwoven fabric between fiber preforms, and subjecting the obtained material and a resin matrix to composite molding by a molding process to obtain a fiber composite material. In the present invention, firstly nanoparticles are uniformly dispersed in a solvent to obtain a nanoparticle dispersion; secondly, the chopped fiber and the nanoparticles cooperate to construct a multi-scale interlaminar toughening phase, which significantly improves the interlaminar fracture toughness of the fiber composite material.

A construct for a hockey blade formed from layers of sheet molding compound material. The sheet molding compound material may be manufactured to have longer average fiber lengths entrained within the sheet molding compound material with random orientation in order to enhance the mechanical properties of the formed hockey stick blade.

A construct for a hockey blade formed from layers of sheet molding compound material. The sheet molding compound material may be manufactured to have longer average fiber lengths entrained within the sheet molding compound material with random orientation in order to enhance the mechanical properties of the formed hockey stick blade.

Stiffened skin panels comprise alternating truss core portions and solid laminate portions sandwiched between inner and outer facesheets, all formed from a fiber reinforced thermoplastic. The components of the panels are co-consolidated using induction heating. The panels are stiffened with spars fastened to the solid laminate portions.

In a first aspect, the disclosure provides; a composite laminate. The laminate is made of: a first exterior layer comprising a biocompatible material; a second exterior layer comprising a biocompatible material; and a first inner layer comprising biocompatible threads running parallel to each other and oriented at zero degrees. The layers are laminated together. The disclosure further provides; a method for creating a biocompatible composite laminate. The method includes laying biocompatible threads parallel to one another to create a first middle thread layer on a first biocompatible material exterior layer, and placing a second biocompatible exterior material layer over the parallel biocompatible threads. The laminate is heated and compressed to bond the layers together.

A method for producing a product including a composite fiber part and a second part, wherein the second part includes a carrier part, wherein the carrier part is a replica of a press tool configured to be heated and to apply a pressure, the method including applying, in a non-cured state, the composite fiber part on the carrier part, arranging the carrier part including the composite fiber part on the press tool, curing the composite fiber part on the carrier part, and removing the product from the press tool, wherein after removal from the press tool the composite fiber part and the carrier part constitutes together at least a part of the finished product. Also disclosed is a composite fiber product including a composite fiber part and a second part.

A method for producing a product including a composite fiber part and a second part, wherein the second part includes a carrier part, wherein the carrier part is a replica of a press tool configured to be heated and to apply a pressure, the method including applying, in a non-cured state, the composite fiber part on the carrier part, arranging the carrier part including the composite fiber part on the press tool, curing the composite fiber part on the carrier part, and removing the product from the press tool, wherein after removal from the press tool the composite fiber part and the carrier part constitutes together at least a part of the finished product. Also disclosed is a composite fiber product including a composite fiber part and a second part.

Methods and systems are provided for fabricating a composite structure. In one example, the composite structure may include a honeycomb core sandwiched between face sheets. An edge of the honeycomb core may be abraded and a top face sheet may be perforated. As such, a likelihood of delamination of the composite structure during a curing step may be reduced.

A non-metallic flange isolation gasket kit sealing flanged pipeline connections and flanged vessel connections while providing electrical isolation protection between flanges suited for high-pressure and high-temperature cathodic protection applications is presented. The invention protects flange faces from media induced corrosion and mitigates flange rotation induced fatigue and failures. The invention comprises of a retainer, a seal, and a seal pre-load structural ring. The seal pre-load structural ring is inserted into the seal, and seal outer diameter surface is joined to the retainer inner diameter surface. A second embodiment comprises of a composite gasket blank, comprising of a retainer and a seal, and a seal pre-load structural ring. The seal outer diameter surface and the retainer inner diameter surface are joined by thermal fusion bonding. The invention may further comprise one or more gasket seating stress stabilizers and/or a centering ring. Tapered retainer upper and lower surfaces decrease flange rotation.