Bulb stiffener with sinusoidal web
An improved composite stiffener and methods and tooling used to form the same. The stiffener includes one or more base flanges, a composite rod extending in an axial direction, a bulb cap surrounding the composite rod, and an upright web extending from the one or more base flanges to the base cap. The upright web includes a non-linear profile in the axial direction providing the improved lateral stiffness. The method includes providing tooling including a first compression tool extending in the axial direction and including a first web portion having a non-linear profile, and a second compression tool extending in the axial direction and including a second web portion having a non-linear profile. Plies are placed within the tooling and compressed such that at least a portion of plurality of plies are compressed in the web forming portion thereby forming a web of the bulb stiffener having a non-linear profile.
1. A method for forming a bulb stiffener, the method comprising:
providing a compression molding apparatus, the compression molding apparatus including a web forming portion having a non-linear profile in an axial direction;
placing a plurality of plies within the compression molding apparatus, with a composite rod placed between at least some of the plurality of plies in the compression molding apparatus; and
compressing the compression molding apparatus such that at least a portion of the plurality of plies are compressed in the web forming portion thereby forming a web of the bulb stiffener having a non-linear profile in the axial direction, wherein the step of compressing the compression molding apparatus further comprises compressing the plurality of plies about an outer perimeter of the composite rod, wherein the composite rod includes a truncated circular cross-sectional profile having a flat portion, and wherein the web extends along a lateral extent of the flat portion.
2. The method of claim 1 , further comprising forming the web of the stringer having a sinusoidal profile in the axial direction.
3. The method of claim 1 , wherein the composite rod is a pultruded rod comprised of zero-degree fibers, and wherein the step of placing the plurality of plies within the compression molding apparatus includes placing a plurality of plies having +/−45-degree fibers in the compression molding apparatus.
4. The method of claim 1 , further comprising heating the plurality of plies prior to placing the plurality of plies within the compression molding apparatus.
5. The method of claim 1 , further comprising:
removing the plurality of plies from the compressing molding apparatus after the plurality of plies solidifies; and
trimming a portion of the plurality of plies.
6. A method for forming a bulb stiffener, the method comprising:
providing a compression molding apparatus, the compression molding apparatus including a web forming portion having a non-linear profile in an axial direction;
placing a plurality of plies within the compression molding apparatus;
placing a composite rod between at least two of the plurality of plies in the compression molding apparatus; and
compressing the compression molding apparatus such that at least a portion of the plurality of plies are compressed in the web forming portion thereby forming a web of the bulb stiffener having a non-linear profile in the axial direction and at least a portion of the plurality of plies are compressed against the composite rod, wherein the composite rod includes a truncated circular cross-sectional profile having a flat portion perpendicular to the web, and wherein the web extends along a lateral extent of the flat portion.
7. The method of claim 6 , further comprising forming the web of the stringer having a sinusoidal profile in the axial direction.
8. The method of claim 6 , wherein the step of placing the composite rod in the compression molding apparatus includes placing a pultruded rod comprised of zero-degree fibers in the compression molding apparatus.
9. The method of claim 6 , wherein the step of placing the plurality of plies within the compression molding apparatus includes placing a plurality of plies having +/−45-degree fibers in the compression molding apparatus.
10. The method of claim 6 , further comprising heating the plurality of plies prior to placing the plurality of plies within the compression molding apparatus.
11. The method of claim 6 , further comprising:
removing the plurality of plies and the composite rod from the compressing molding apparatus after the plurality of plies solidifies; and
trimming a portion of the plurality of plies.