B29B11/00

Method and apparatus for producing fiber-reinforced resin molding material

Provided are a method and an apparatus for manufacturing a fiber-reinforced resin molding material by which, when the fiber-reinforced resin molding material is manufactured, separated fiber bundles can be supplied to a cutting machine in stable condition while avoiding the influence of meandering of the fiber bundles or slanting or meandering of filaments occurring in the fiber bundles. A method for manufacturing a sheet-shaped fiber-reinforced resin molding material in which spaces between filaments of cut-out fiber bundles (CF) are impregnated with resin includes, so that a condition of the following expression (1) is satisfied, intermittently separating fibers of the continuous fiber bundles (CF) in a longitudinal direction by a rotational blade (18) serving as a fiber separating part and cutting out the fiber bundles with an interval therebetween in a longitudinal direction of a cutting machine (13A) to obtain the cut-out fiber bundles (CF). Expression (1): 1?a/L (where a represents a length of a separated part of the continuous fiber bundles (CF) and L represents an interval when the fiber bundles (CF) are cut out in the longitudinal direction.)

Method for producing shaping material
11905380 · 2024-02-20 · ·

Provided is a method for producing a shaping material that contains a cyclic olefin polymer and has a low content of a volatile impurity. This method for producing a shaping material is a method which includes passing a raw-material resin in a molten state through an extruder to produce a shaping material, and in which the extruder is equipped with a cylinder, a screw housed within the cylinder, a resin introduction port for introducing the raw-material resin into the cylinder, a resin discharge port for discharging the molten resin from the cylinder, a fluid injection port for injecting carbon dioxide or water into the cylinder between the resin introduction port and the resin discharge port, and a fluid discharge port for removing fluid in the cylinder by suction downstream of the fluid injection port and between the resin introduction port and the resin discharge port.

PREFORM FIGURING METHOD, COMPOSITE MATERIAL SHAPING METHOD, COMPOSITE MATERIAL, AND AIRCRAFT STRUCTURAL PART
20190275754 · 2019-09-12 ·

A preform figuring method includes mounting and stacking sheet-shape fibrous preparations that have been or are yet to be impregnated with a thermosetting resin on a figuring die that has first and second figuring surfaces at least either one of which is a curved surface and making a preform for a composite material which has a curved surface that corresponds to the curved surface of the figuring die as a stack of the fibrous preparations which has layers by bending the fibrous preparations mounted on the first figuring surface onto the second figuring surface. At least a fraction of the layers that constitute the stack are formed by mounting sheet-shape fibrous preparations on the first figuring surface or the fibrous preparation adjacent in a stacking direction so that the fibrous preparations partly overlap and bending portions of the fibrous preparations mounted so as to overlap onto the second figuring surface.

PREFORM FIGURING METHOD, COMPOSITE MATERIAL SHAPING METHOD, COMPOSITE MATERIAL, AND AIRCRAFT STRUCTURAL PART
20190275754 · 2019-09-12 ·

A preform figuring method includes mounting and stacking sheet-shape fibrous preparations that have been or are yet to be impregnated with a thermosetting resin on a figuring die that has first and second figuring surfaces at least either one of which is a curved surface and making a preform for a composite material which has a curved surface that corresponds to the curved surface of the figuring die as a stack of the fibrous preparations which has layers by bending the fibrous preparations mounted on the first figuring surface onto the second figuring surface. At least a fraction of the layers that constitute the stack are formed by mounting sheet-shape fibrous preparations on the first figuring surface or the fibrous preparation adjacent in a stacking direction so that the fibrous preparations partly overlap and bending portions of the fibrous preparations mounted so as to overlap onto the second figuring surface.

Thermoplastic bonded preforms and thermoset matrices formed therewith
10406776 · 2019-09-10 · ·

A thermoplastic bonded preform and method of manufacturing the preform are disclosed. The preform comprises a primary fiber comprising little or no sizing; a mechanical fiber; and a thermoplastic.

Thermoplastic bonded preforms and thermoset matrices formed therewith
10406776 · 2019-09-10 · ·

A thermoplastic bonded preform and method of manufacturing the preform are disclosed. The preform comprises a primary fiber comprising little or no sizing; a mechanical fiber; and a thermoplastic.

Thermoplastic Bonded Preforms and Thermoset Matrices Formed Therewith
20190263085 · 2019-08-29 · ·

A thermoplastic bonded preform and method of manufacturing the preform are disclosed. The preform comprises a primary fiber comprising little or no sizing; a mechanical fiber; and a thermoplastic.

Thermoplastic Bonded Preforms and Thermoset Matrices Formed Therewith
20190263085 · 2019-08-29 · ·

A thermoplastic bonded preform and method of manufacturing the preform are disclosed. The preform comprises a primary fiber comprising little or no sizing; a mechanical fiber; and a thermoplastic.

Systems for additively manufacturing composite parts

A system for additively manufacturing a composite part comprises a delivery guide, movable relative to a surface. The delivery guide is configured to deposit at least a segment of a continuous flexible line along a print path. The continuous flexible line comprises a non-resin component and a thermosetting-resin component. The thermosetting-resin component comprises a first part and a second part. The non-resin component comprises a first element and a second element. The system further comprises a first resin-part applicator, configured to apply the first part to the first element, and a second resin-part applicator, configured to apply the second part to the second element. The system also comprises a feed mechanism, configured to pull the first element through the first resin-part applicator, to pull the second element through the second resin-part applicator, and to push the continuous flexible line out of the delivery guide.

Systems for additively manufacturing composite parts

A system for additively manufacturing a composite part comprises a delivery guide, movable relative to a surface. The delivery guide is configured to deposit at least a segment of a continuous flexible line along a print path. The continuous flexible line comprises a non-resin component and a thermosetting-resin component. The thermosetting-resin component comprises a first part and a second part. The non-resin component comprises a first element and a second element. The system further comprises a first resin-part applicator, configured to apply the first part to the first element, and a second resin-part applicator, configured to apply the second part to the second element. The system also comprises a feed mechanism, configured to pull the first element through the first resin-part applicator, to pull the second element through the second resin-part applicator, and to push the continuous flexible line out of the delivery guide.