Composite inlet guide vane
A composite vane includes an airfoil portion having an inner core composed primarily of fiberglass epoxy; a carbon epoxy fabric located outward of the inner core; a relatively thin layer of fiberglass epoxy, and an outer metal sheath.
1. A composite vane comprising an airfoil portion having an inner core composed primarily of fiberglass epoxy: said inner core surrounded by a continuous fiber reinforced carbon epoxy fabric; said continuous fiber reinforced carbon epoxy fabric surrounded by a fiberglass epoxy layer and an outer metal sheath bonded to said fiberglass epoxy layer.
2. The composite vane of claim 1 wherein said airfoil portion is comprised of between about 15-30% by volume of said carbon/epoxy fabric.
3. The composite airfoil of claim 2 wherein said outer metal sheath comprises aluminum.
4. The composite airfoil of claim 2 wherein said outer metal sheath comprises an aluminum coating.
5. The composite vane of claim 2 wherein fiber orientation in said carbon/epoxy fabric is radial chord-wise ±45°.
6. The composite vane of claim 1 wherein said vane comprises a compressor inlet guide vane.
7. The composite vane of claim 2 wherein said carbon/epoxy fabric is located nearer peripheral external surfaces of said airfoil than to a center of said inner core.
8. The composite vane of claim 3 wherein said aluminum sheath has a thickness of about 0.010 inch.
9. The composite vane of claim 1 wherein said metal sheath is comprised of cold-spray-deposited 7000 series aluminum.
10. The composite vane of claim 3 wherein said aluminum sheath is coated with a phosphate/chromate sealer.
11. The composite vane of claim 1 and further comprising a spindle attached to said airfoil portion.
12. A composite vane comprising an airfoil portion having an inner core composed primarily of fiberglass epoxy and an outer metal sheath surrounding said inner core, and further comprising a spindle attached to said airfoil portion and wherein said airfoil portion is formed at its radially inner end with a tab adapted to be received in a recess provided in said spindle and wherein said tab is comprised of a pair of aluminum tab portions on either side of a fiberglass epoxy tab portion and wherein said aluminum and fiberglass epoxy tab portions have a rectangular cross-sectional shape.
13. A composite vane for a compressor comprising an airfoil portion having an inner core composed primarily of fiberglass epoxy and an outer metal sheath, wherein said airfoil portion is further comprised of about 20% by volume of carbon/epoxy fabric located in selected areas of said airfoil portion outwardly of said inner core, and wherein additional fiberglass epoxy material is interposed between said carbon/epoxy fabric and said outer metal sheath; and wherein said airfoil portion is formed at its radially inner end with a composite tab adapted to be received in a pocket provided in said spindle, said composite tab comprising fiberglass epoxy sandwiched between extensions of said outer metal sheath.
14. The composite airfoil of claim 13 wherein said outer metal sheath comprises aluminum.
15. The composite airfoil of claim 13 wherein said outer metal sheath comprises an aluminum coating.