The invention relates to a method for manufacturing a composite aircraft window frame; the method comprises the steps of: a) positioning in a mold a preform made of pre-impregnated material including dispersed fibers, with a predefined orientation, in a thermosetting resin matrix; b) closing the mold so as to define a gap between at least one surface of said preform and a portion of said mold; c) injecting thermosetting resin into the closed mold through an inlet opening of the mold itself, so as to fill the gap and completely lap said surface of the preform; and d) applying a uniform hydrostatic pressure on the surface by the injection of the resin.

The invention relates to a method for manufacturing a composite aircraft window frame; the method comprises the steps of: a) positioning in a mold a preform made of pre-impregnated material including dispersed fibers, with a predefined orientation, in a thermosetting resin matrix; b) closing the mold so as to define a gap between at least one surface of said preform and a portion of said mold; c) injecting thermosetting resin into the closed mold through an inlet opening of the mold itself, so as to fill the gap and completely lap said surface of the preform; and d) applying a uniform hydrostatic pressure on the surface by the injection of the resin.

A composite rebar having ridges formed therein by grinding is buffed and/or coated to reduce the surface roughness caused by fibers extending from the rebar.

A composite panel including a vibration suppression layer includes: a rubber material; a first structure material layer positioned on the vibration suppression layer and including a fiber reinforced plastic (FRP); and a second structure material layer positioned under the vibration suppression layer and including a fiber reinforced plastic.

A molding jig for molding a laminate, which includes reinforced fiber sheets laminated on each other, extends in the length direction, and has a cross-sectional shape having a curved portion in a cross section obtained by cutting the laminate on a plane orthogonal to the length direction, into a three-dimensional shape having a bent portion in the length direction. The molding jig includes a female die for forming the bent portion, a male die for engaging with the female die with the laminate therebetween for forming the bent portion, and a stretchable supporting member between the female die and the laminate. The laminate comes in contact with the male die on both length-direction sides of the molded bent portion, and the supporting member is over a region including the female-side molding surface.

A molding jig for molding a laminate, which includes reinforced fiber sheets laminated on each other, extends in the length direction, and has a cross-sectional shape having a curved portion in a cross section obtained by cutting the laminate on a plane orthogonal to the length direction, into a three-dimensional shape having a bent portion in the length direction. The molding jig includes a female die for forming the bent portion, a male die for engaging with the female die with the laminate therebetween for forming the bent portion, and a stretchable supporting member between the female die and the laminate. The laminate comes in contact with the male die on both length-direction sides of the molded bent portion, and the supporting member is over a region including the female-side molding surface.

Methods and apparatus for additive manufactures of complex parts using co-aligned continuous fibers are disclosed. Filament subunits having complex shapes are fabricated and inserted into a mold cavity. The layup is compression molded to form a complex part having high tensile strength.

In a method for producing fiber-reinforced plastic parts in a mold and an adhesive layer for carrying out the method, the adhesive layer adhesive force on the mold is greater than the adhesive layer adhesive force on the segment, so that, after a first segment is removed, the adhesive layer remains completely in the mold and after the temperature of the adhesive layer is increased through contact with a melted plastic matrix, the remaining adhesive force is sufficient to adhere at least a second segment. The adhesive layer, introduced into the mold relatively expensively, and removed from the mold and disposed of at further expense, is used repeatedly, not just for a single adhesion operation. The expense for procuring the adhesive layer, its introduction into the mold, removal and disposal remains but through its division over numerous production operations, the total expenditure proportion for each operation decreases dramatically.

In a method for producing fiber-reinforced plastic parts in a mold and an adhesive layer for carrying out the method, the adhesive layer adhesive force on the mold is greater than the adhesive layer adhesive force on the segment, so that, after a first segment is removed, the adhesive layer remains completely in the mold and after the temperature of the adhesive layer is increased through contact with a melted plastic matrix, the remaining adhesive force is sufficient to adhere at least a second segment. The adhesive layer, introduced into the mold relatively expensively, and removed from the mold and disposed of at further expense, is used repeatedly, not just for a single adhesion operation. The expense for procuring the adhesive layer, its introduction into the mold, removal and disposal remains but through its division over numerous production operations, the total expenditure proportion for each operation decreases dramatically.

A fiber composite structure includes a base structure being formed of a first fiber composite material that includes first fiber bundles embedded in a first matrix material, wherein the base structure includes an opening defined by first fiber bundles which include first sections and a second section that continuously or uninterruptedly interconnects the first sections, wherein the second section forms a bay that defines a part of the circumference of the opening. The fiber composite structure further includes a functional structure positioned in the opening of the base structure and joined with the first fiber composite material of the base structure.