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US 2026/0192529 A1Published application
Recycled Resin Infusion Radius Filler and Method
AssigneeThe Boeing Company
InventorsMarcus Charles Hart, Christopher Robert Loesche
Life of this patent
Estimating the term…
Abstract
A tailorable composite material longitudinal radius filler made from harvested, recycled dry fiber material and a composite material assembly a longitudinal radius filler cavity filled with the tailorable composite material longitudinal radius filler and methods of manufacture are presently disclosed herein.
Claims20
A composite material assembly comprising:
- at least one composite material assembly member comprising a dry fiber material impregnated with an epoxy resin-containing material, said at least one composite material assembly member comprising:
- a composite material assembly member first side;
- a composite material assembly member second side;
- a longitudinal radius filler cavity bounded by the composite material
- assembly member second side, said longitudinal radius filler cavity comprising a longitudinal cavity radius;
- and
- a tailorable composite material longitudinal radius filler positioned within the longitudinal radius filler cavity, said tailorable composite material longitudinal radius filler comprising a tailorable composite material longitudinal radius filler radius dimensioned to substantially match the longitudinal cavity radius, said tailorable composite material longitudinal radius filler comprising a recycled dry fiber material impregnated with the epoxy resin-containing material.
4 more elements
A method for forming a tailorable composite material longitudinal radius filler, the method comprising:
- harvesting an amount of a waste dry fiber material from a separate composite material formation process;
- forming a recycled dry fiber material from the waste dry fiber material:
- tooling the recycled dry fiber material to form the tailorable composite material longitudinal radius filler;
- impregnating the recycled dry fiber material with a resin-containing material to form a curable composite material longitudinal radius filler;
- and
- curing the curable composite material longitudinal radius filler to form a cured composite material longitudinal radius filler configured to comprise a selected stiffness.
3 more elements
A method of making a composite material assembly comprising a composite material longitudinal radius filler, the method comprising:
- providing at least one composite material assembly member, said at least one composite material assembly member comprising a composite material assembly member first side and a composite material assembly member second side, said composite material assembly member further comprising a longitudinal radius filler cavity bounded by the composite material assembly member second side, said longitudinal radius filler cavity comprising a longitudinal cavity radius, said at least one composite material assembly member comprising a first stiffness value, said composite material assembly member comprising a dry fiber material impregnated with a resin-containing material to form the composite material assembly member;
- positioning a tailorable composite material longitudinal radius filler in the longitudinal radius filler cavity to form the composite material assembly, said tailorable composite material longitudinal radius filler comprising a recycled dry fiber material impregnated with a resin-containing material to form the tailorable composite material longitudinal cavity filler, said tailorable composite material longitudinal radius filler comprising a radius filler longitudinal radius configured to substantially match the longitudinal cavity radius, said tailorable composite material longitudinal radius filler configured to completely fill the longitudinal radius filler cavity, said tailorable composite material longitudinal radius filler comprising a second stiffness value;
- forming the composite material assembly;
- wherein the recycled dry fiber material comprises a tailored form of the dry fiber material;
- and
- wherein a stiffness ratio of the first stiffness value to the second stiffness value is a stiffness ratio ranging from about 1:6 to about 6:1.
3 more elements
Dependencies are inferred from the claim text.