Composite parts, and methods of manufacturing
A method for manufacturing a composite part includes forming an initial radius filler on a composite panel. The initial radius filler is formed from a plurality of plies of composite material stacked on the composite panel. The method includes forming a radius of curvature on at least one side of the initial radius filler, positioning a composite stiffener on the composite panel, wherein the composite stiffener is contoured to define a radius gap when joined with the composite panel, positioning the composite stiffener against the at least one side of the initial radius filler, compressing the composite stiffener, composite panel, and initial radius filler via vacuum bag, and heating the initial radius filler to at least one of a cure temperature, a melting temperature, or a fusing temperature to form, from the initial radius filler, a radius gap filler in the radius gap.
1. A method of manufacturing a composite part, the method comprising:
forming an initial radius filler on a composite panel, wherein the initial radius filler is formed from a plurality of plies of composite material stacked on the composite panel;
forming a radius of curvature on at least one side of the initial radius filler;
positioning a composite stiffener on the composite panel, wherein the composite stiffener is contoured to define a radius gap when joined with the composite panel;
positioning the composite stiffener against the at least one side of the initial radius filler;
compressing the composite panel and the composite stiffening member together via consolidation pressure; and
heating the initial radius filler to at least one of a cure temperature, a melting temperature, or a fusing temperature to form, from the initial radius filler, a radius gap filler in the radius gap;
wherein forming the radius of curvature includes size-reducing the at least one side of the initial radius filler.
2. The method of claim 1 , wherein forming the initial radius filler includes co-forming the composite panel and the initial radius filler from plies of composite material on the same tool.
3. The method of claim 2 , wherein at least one ply of the initial radius filler is positioned between two plies of the composite panel.
4. The method of claim 2 , wherein at least one ply of the composite panel and of the initial radius filler have different fiber orientations relative to each other.
5. The method of claim 1 , wherein at least one ply of the initial radius filler has a different fiber orientation relative to the other plies of the initial radius filler.
6. The method of claim 1 , wherein forming the radius of curvature includes offsetting the stacking of the plurality of plies.
7. The method of claim 1 , wherein forming the initial radius filler includes:
laying down a first group of plies in a first stack on the composite panel; and
laying down a second group of plies in a second stack on the first group of plies, wherein the plies in the second group have a lesser width than the plies in the first group.
8. The method of claim 1 , wherein forming the initial radius filler includes performing automated fiber placement of the plurality of plies of composite material.
9. The method of claim 1 , wherein forming the initial radius filler includes forming the plurality of plies from continuous strips of composite material.
10. A method of manufacturing a composite part, the method comprising:
forming an initial radius filler on a composite panel, wherein the initial radius filler is formed from a plurality of plies of composite material stacked on the composite panel;
forming a radius of curvature on at least one side of the initial radius filler;
positioning a composite stiffener on the composite panel, wherein the composite stiffener is contoured to define a radius gap when joined with the composite panel;
positioning the composite stiffener against the at least one side of the initial radius filler;
compressing the composite panel and the composite stiffening member together via consolidation pressure; and
heating the initial radius filler to at least one of a cure temperature, a melting temperature, or a fusing temperature to form, from the initial radius filler, a radius gap filler in the radius gap;
wherein forming the initial radius filler includes forming the plurality of plies from continuous strips of composite material;
wherein the continuous strips include unidirectional fibers oriented in the length dimension of the radius gap filler.
11. A method of manufacturing a composite part, the method comprising:
determining an install location for at least one stiffener on a composite panel;
forming an initial radius filler at the install location on the composite panel, wherein the initial radius filler is formed from a plurality of plies of composite material;
positioning a composite stiffener on the composite panel, wherein the composite stiffener is contoured to define a radius gap when joined with the composite panel;
using the initial radius filler to position the composite stiffener at the install location;
compressing the composite panel and the composite stiffening member together via consolidation pressure;
heating the initial radius filler to at least one of a cure temperature, a melting temperature, or a fusing temperature to form, from the initial radius filler, a radius gap filler in the radius gap;
forming a radius of curvature on at least one side of the initial radius filler, wherein the composite stiffener is positioned against the at least one side of the initial radius filler
wherein forming the radius of curvature includes size-reducing the at least one side of the initial radius filler to a pre-formed shape.
12. The method of claim 11 , wherein forming the radius of curvature includes laying down a subsequently laid ply of composite material at an offset from at least one previously laid ply of composite material.