Composite tubular structure
US-2019128449-A1 · May 2, 2019 · US
US10927883B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10927883-B2 |
| Application number | US-201715646506-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 11, 2017 |
| Priority date | Jul 11, 2017 |
| Publication date | Feb 23, 2021 |
| Grant date | Feb 23, 2021 |
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A composite tube may include a body having a longitudinal centerline axis and an end portion having a tapered section and an end rim. At least one of a radially outward edge and a radially inward edge of the end rim may be non-circular. The end rim may be circumferentially continuous. The end rim may be an undulating annulus. A joint assembly may include a support wedge that at least partially engages at least one of a radially inward surface of the end portion and a radially outward surface of the end portion of the composite tube.
Opening claim text (preview).
What is claimed is: 1. A composite tube comprising: a body comprising a longitudinal centerline axis; and an end portion comprising a tapered section terminating at an end rim, wherein one of a radially outward edge and a radially inward edge of the end rim is non-circular and the other of the radially outward edge and the radially inward edge is circular; wherein the end rim is circumferentially continuous; wherein the end rim is an undulating annulus; wherein the one of the radially outward edge and the radially inward edge of the end rim comprises an undulating wave-like shape; wherein the tapered section comprises a plurality of folds that form circumferentially distributed grooves extending along the tapered section; and wherein the circumferentially distributed grooves are shorter than the tapered section, as measured in a direction along the longitudinal centerline axis, such that the circumferentially distributed grooves terminate on the tapered section. 2. The composite tube of claim 1 , wherein the tapered section converges radially inward in a direction from the body to the end rim. 3. The composite tube of claim 1 , wherein the body comprises a circular cross-section. 4. A joint assembly comprising: a composite tube comprising a body having a longitudinal centerline axis and an end portion comprising an end rim that is circumferentially continuous, wherein a radially inward edge of the end rim is non-circular and a radially outward edge of the end rim is circular; and a support wedge that at least partially engages a radially inward surface of the end portion, wherein the radially inward surface comprises an undulating shape of the end portion. 5. The joint assembly of claim 4 , wherein the end portion of the composite tube comprises a tapered section that converges radially inward in a direction from the body to the end rim, wherein the radially inward surface and a radially outward surface are walls of the tapered section of the end portion. 6. The joint assembly of claim 5 , wherein the tapered section comprises a plurality of folds that form circumferentially distributed grooves extending along the tapered section, wherein the circumferentially distributed grooves impart the undulating shape to the end portion. 7. The joint assembly of claim 6 , wherein the support wedge comprises contours that complement the circumferentially distributed grooves of the tapered section. 8. The joint assembly of claim 7 , wherein the end rim is an undulating annulus. 9. The joint assembly of claim 8 , wherein the support wedge is a first support wedge, wherein the joint assembly further comprises a second support wedge that engages the radially outward surface. 10. The joint assembly of claim 9 , wherein the second support wedge is an external support wedge that has an annular structure that is concentric with the longitudinal centerline axis and that circumscribes the end portion of the composite tube. 11. A method of forming a joint assembly, the method comprising: forming an end portion of a composite tube, wherein the end portion comprises an end rim, wherein a radially inward edge of the end rim is non-circular and a radially outward edge is circular; engaging a support wedge to the end portion of the composite tube, wherein the support wedge comprises contours that complement the end portion; and after engaging the support wedge to the end portion of the composite tube, curing or solidifying the composite tube. 12. The method of claim 11 , wherein forming the end portion comprises tapering the end portion of the composite tube to form a tapered section that converges radially inward in a direction from a body of the composite tube to the end rim. 13. The method of claim 11 , wherein forming the end portion comprises shaping the end portion to have a plurality of folds that form circumferentially distributed grooves along a radially inward surface of the end portion. 14. The method of claim 13 , wherein shaping the end portion comprises using the support wedge as a mold. 15. The method of claim 14 , wherein the support wedge is an internal support wedge, wherein the method further comprises engaging an annular external support wedge to the end portion.
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