Systems and methods for forming a composite structure
The present disclosure provides systems and methods for forming a composite structure comprising rotating a base layer of an apparatus for forming the composite structure about an axis of rotation, transferring carbon short fibers from a first vibratory feed ramp onto the base layer in order to form a plurality of fibrous layers in the composite structure, and vibrating the first vibratory feed ramp during the transferring the carbon short fibers. The base layer may comprise an annular shape.
1. A method for making a composite structure, comprising:
rotating a base layer of an apparatus for forming the composite structure about an axis of rotation;
transferring carbon short fibers from a first vibratory feed ramp onto the base layer in order to form a plurality of fibrous layers in the composite structure;
vibrating the first vibratory feed ramp during the transferring the carbon short fibers; and
transferring additional carbon short fibers from a supplemental vibratory feed ramp onto an outer diameter area of the base layer,
wherein the base layer comprises an annular shape.
2. The method of claim 1 , further comprising cutting a carbon fiber strand into the carbon short fibers, wherein the carbon short fibers are between 0.5 inch and 2 inches in length.
3. The method of claim 1 , further comprising cutting a carbon fiber strand into the carbon short fibers, wherein the carbon short fibers are between 0.75 inch and 1.5 inches in length.
4. The method of claim 1 , further comprising transferring the carbon short fibers from a first loader onto the first vibratory feed ramp, wherein the first loader comprises a loader hole comprising a first dimension and a second dimension, wherein the first dimension is larger than the second dimension, and the first dimension transfers the carbon short fibers to an outer edge of the first vibratory feed ramp.
5. The method of claim 1 , further comprising rolling the carbon short fibers with a roller in response to the transferring the carbon short fibers.
6. The method of claim 1 , further comprising compressing each of the plurality of fibrous layers during the rotating the base layer at a compression zone of the apparatus.
7. The method of claim 6 , further comprising disposing an inner sacrificial edge along an inner diameter of the base layer and an outer sacrificial edge along an outer diameter of the base layer.
8. The method of claim 6 , wherein the compressing comprises needling each of the plurality of fibrous layers during the rotating the base layer at the compression zone of the apparatus.
9. The method of claim 1 , further comprising transferring a secondary material from a second vibratory feed ramp onto the base layer of the apparatus, and vibrating the second vibratory feed ramp during the transferring the secondary material, wherein the secondary material comprises at least one of ceramic particles, powdery resin, carbon particles, or graphite particles.
10. The method of claim 9 , wherein the transferring the carbon short fibers and the transferring the secondary material occur simultaneously.
11. The method of claim 1 , further comprising densifying the carbon structure by at least one of chemical vapor infiltration, pre-ceramic polymer infiltration, or silicon melt infiltration.
12. The method of claim 1 , wherein the base layer is disposed within a cavity having an annular shape.
13. The method of claim 12 , further comprising:
transferring a secondary material from a second vibratory feed ramp into the cavity; and
vibrating the second vibratory feed ramp during the transferring the secondary material.
14. The method of claim 13 , wherein the secondary material comprises at least one of ceramic particles, powdery resin, carbon particles, or graphite particles.
15. The method of claim 12 , further comprising pretreating a carbon fiber strand to form an interface coating on the carbon fiber strand comprising at least one of pyrolytic carbon, boron nitride, or silicon carbide, wherein the carbon fiber strand is cut into the carbon short fibers.
16. The method of claim 12 , further comprising cutting a carbon fiber strand to form the carbon short fibers, wherein the carbon short fibers are between 0.5 inch and 2 inches in length.
17. The method of claim 12 , further comprising compressing each of the plurality of fibrous layers during the rotating the base layer at a compression zone of the apparatus.
18. The method of claim 13 , further comprising densifying the carbon structure by at least one of chemical vapor infiltration, pre-ceramic polymer infiltration, or silicon melt infiltration.
19. A method for making a composite structure, comprising:
rotating a base layer of an apparatus for forming the composite structure about an axis of rotation;
transferring carbon short fibers from a first vibratory feed ramp onto the base layer in order to form a plurality of fibrous layers in the composite structure;
vibrating the first vibratory feed ramp during the transferring the carbon short fibers; and
transferring the carbon short fibers from a first loader onto the first vibratory feed ramp, wherein the first loader comprises a loader hole comprising a first dimension and a second dimension, wherein the first dimension is larger than the second dimension, and the first dimension transfers the carbon short fibers to an outer edge of the first vibratory feed ramp,
wherein the base layer comprises an annular shape.