Integrally woven composite fan blade using progressively larger weft yarns
A composite blade includes a preform and a binder. The preform is a preform of yarns woven in three-dimensions and has a tip region, a root region and an intermediate region. The intermediate region is positioned between the tip region and the root region. The yarns comprise warp yarns and weft yarns. The warp yarns form a longitudinal axis. The weft yarns are positioned at a 90 degree angle to the warp yarns. The weft yarns increase in yarn size as determined by filament count along the longitudinal axis to change the thickness of the preform. The binder maintains the relative positions of the preform yarns.
1. A method of forming a composite blade, the method comprising:
three-dimensionally weaving warp yarns and weft yarns to form a three-dimensional preform, wherein the warp yarns form a longitudinal axis and wherein the weft yarns are arranged in increasing or decreasing yarn size as determined by filament count along the longitudinal axis to vary the thickness of the preform and wherein the preform has a substantially uniform weave pattern and a substantially constant number of weft yarns per column unit throughout the preform;
inserting the preform into a mold;
injecting the mold with resin for maintaining the relative positions of the yarns; and
curing the resin.
2. The method of claim 1 , wherein the preform has a tip and a root and wherein the weft yarns of the root are arranged to increase in yarn size with increasing distance from the tip.
3. The method of claim 2 , wherein the root has a dovetail taper.
4. The method of claim 1 , wherein the preform has a uniform weave pattern throughout.
5. A composite blade comprising:
a preform of yarns woven in three-dimensions, the preform having a tip region, a root region and an intermediate region positioned between the tip region and the root region, and the yarns comprising:
warp yarns forming a longitudinal axis of the preform; and
weft yarns positioned at a 90 degree angle to the warp yarns, wherein the weft yarns increase in yarn size as determined by filament count along the longitudinal axis to change the thickness of the preform; and
a binder maintaining the relative positions of the preform yarns, wherein the preform has a substantially uniform weave pattern and a substantially constant number of weft yarns per column unit throughout the preform.
6. The composite blade of claim 5 , wherein the root region of the preform has a divergent shape such that the thickness of the preform increases in the root region with increasing distance from the tip region, and wherein the yarn size of the weft yarns increases in the root region along the longitudinal axis with increasing distance from the tip region.
7. The composite blade of claim 6 , wherein the root region has a dovetail taper shape.
8. The composite blade of claim 5 , wherein the yarn size of the weft yarns in the root region are greater than the yarn size of the weft yarns in the intermediate region.
9. The composite blade of claim 5 , wherein the yarn size of the weft yarns in the root region are greater than a yarn size as determined by filament count of the warp yarns in the root region.
10. The composite blade of claim 5 , wherein each warp yarn has a yarn size as determined by filament count equal to a first value.
11. The composite blade of claim 5 , wherein the root region, the intermediate region and the tip region of the preform have a first weave pattern.
12. The composite blade of claim 5 , wherein the weft yarns are uniformly spaced along the longitudinal axis.
13. The composite blade of claim 5 , wherein the root region and the intermediate region contain repeating column units of weft yarns, and wherein the root region contains a same number of weft yarns per column unit as the intermediate region.
14. The composite blade of claim 5 , wherein in each plane of the composite blade, the root region contains a same number of warp yarns as the intermediate region.
15. The composite blade of claim 5 , wherein a portion of the preform changes between about 0.5 cm and about 2.5 cm in thickness per cm of length.
16. A composite blade comprising:
a preform of yarns woven in three-dimensions with a substantially uniform weave pattern, the preform having a tip, a root and an intermediate region positioned between the tip and the root, and the yarns comprising:
warp yarns forming a spanwise axis of the preform; and
weft yarns positioned at a 90 degree angle to the warp yarns, wherein the weft yarns vary in yarn size as determined by filament count along the spanwise axis to change the thickness of the preform and wherein the number of weft yarns per column unit is substantially constant throughout the preform;
laminate sections located on either side of the preform and defining the outer surface of the blade and
a binder maintaining the relative positions of the preform yarns.
17. The composite blade of claim 16 , wherein the diameter of the weft yarns increases along the spanwise axis with increasing distance from the tip.
18. The composite blade of claim 16 , wherein the weft yarns are uniformly spaced in the spanwise direction.
19. The composite blade of claim 16 , wherein the preform has a uniform weave pattern extending from the root to the tip.
20. The composite blade of claim 16 , wherein the weft yarns include at least one of the following: graphite fibers, silicone carbide fibers, glass fibers and boron fibers and combinations thereof.