Implant fusion device and method of manufacturing
US-2024423813-A1 · Dec 26, 2024 · US
US10220605B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10220605-B2 |
| Application number | US-201514936870-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 10, 2015 |
| Priority date | Nov 10, 2015 |
| Publication date | Mar 5, 2019 |
| Grant date | Mar 5, 2019 |
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Systems and methods are provided for curing composite products. One exemplary embodiment is an edge breather for composite manufacturing. The edge breather is formed of a rigid material and includes an elongated body having a top open structure with a cross section that defines an arch. The edge breather also includes hollow passageways within the elongated body that are underneath the top structure and travel along a length of the elongated body. The top open structure defines multiple openings forming an open mesh through which air may enter.
Opening claim text (preview).
The invention claimed is: 1. An apparatus comprising: an edge breather for composite manufacturing, formed of a rigid material and comprising: an elongated body having a top open structure with a cross section that defines an arch; hollow passageways within the elongated body that are underneath the top structure and travel along a length of the elongated body; the top structure defines multiple openings forming an open mesh through which air may enter; a base; a plurality of support members protruding from the base, each support member comprising a portion proximate to the base and a portion distal from the base; and a plurality of lateral members interconnecting the distal portions of the support members, forming the top structure. 2. The edge breather of claim 1 , wherein: the support members are linear and rigid. 3. The edge breather of claim 1 , wherein: the top structure is configured to distribute load to the support members to place the support members in compression, while also distributing load to the lateral members to place at least one of the lateral members in tension. 4. The edge breather of claim 1 , wherein: the top structure arcs over the base. 5. The edge breather of claim 1 , wherein: the support members each protrude at an angle from the base, and the angle of each of the support members is determined based on the proximity of the support member to an edge the base, and the angle of each support member ensures that the support member experiences column compression and counteracts crushing forces applied to the top structure of the edge breather during fabrication of a part. 6. The edge breather of claim 1 , further comprising: a second plurality of lateral members interconnecting distal portions of the support members, forming a second open structure above the base. 7. The edge breather of claim 1 , further comprising: a wall defining a hollow cylindrical tunnel continuing through a center of the base. 8. The edge breather of claim 6 , further comprising: a plurality of support members protruding from the wall. 9. The edge breather of claim 6 , further comprising: a flow meter configured to measure airflow through the edge breather. 10. The edge breather of claim 6 , wherein: the base, support members, and lateral members are integral. 11. The edge breather of claim 1 , wherein: the base, support members, and lateral members are integral, and the edge breather is fabricated via printing from a three dimensional (3D) printer. 12. The edge breather of claim 1 , wherein: the top structure comprises a lattice. 13. The edge breather of claim 1 , wherein: the edge breather is coupled with a vacuum line that draws gases from a curing composite product through the edge breather and into the vacuum line. 14. A composite manufacturing system comprising: a rigid tool having a surface configured to support a composite material part; an edge breather atop the rigid tool, comprising: a base; a plurality of support members protruding from the base; and a plurality of lateral members interconnecting portions of the support members that are distal from the base, forming a top structure over the base that defines an arch covering at least one hollow passageway; a surface breather laid atop the edge breather; and a vacuum bag sealing the edge breather, the surface breather, and a portion of the tool from surrounding atmosphere. 15. The system of claim 14 , wherein: the support members are linear and rigid. 16. The system of claim 14 , wherein: the support members each protrude at an angle from the base, and the angle of each of the support members is determined based on the proximity of the support member to an edge of the base. 17. The system of claim 14 , further comprising: a second plurality of lateral members interconnecting distal portions of the support members, forming a second top structure above the base. 18. The system of claim 14 , wherein the edge breather further comprises: a wall defining a hollow cylindrical tunnel continuing through a center of the base. 19. The system of claim 18 , further comprising: a plurality of support members protruding from the tunnel. 20. The system of claim 18 , further comprising: a flow meter configured to measure airflow through the edge breather. 21. The system of claim 14 , wherein: the base, support members, and lateral members are integral. 22. The system of claim 14 , wherein: the open patterned structure comprises a lattice. 23. The system of claim 14 , wherein: the top structure is configured to distribute load to the support members to place the support members in compression, while also distributing load to the lateral members to place at least one of the lateral members in tension. 24. A method for fabricating a composite product, comprising: placing a composite charge on a tool; locating edge breathers along the perimeter of the composite charge; creating a vacuum chamber around the charge and edge breathers; drawing a vacuum in the vacuum chamber; and drawing gases from the composite charge past support members protruding from a base of the edge breathers and underneath lateral members that are interconnected with portions of the support members which are distal from the base, and which form a top structure over the base that defines an arch covering at least one hollow passageway. 25. The method of claim 24 , further comprising: positioning a surface breather atop the composite charge and the edge breathers. 26. The method of claim 24 , further comprising: curing the composite charge. 27. The method of claim 24 wherein: drawing gases past the support member comprises drawing gases past a plurality of support members that each protrude from the base and support an open patterned structure. 28. The method of claim 27 wherein: the edge breathers exhibit an arch shaped cross-section through which gases may freely enter or exit the edge breathers. 29. The method of claim 24 , further comprising: applying a parting film atop the composite charge. 30. The method of claim 24 , further comprising: placing the support member of an edge breather in compression while placing a lateral member of the edge breather in tension, when drawing a vacuum in the vacuum chamber. 31. A method for fabricating an edge breather, comprising: heating a structural material into a liquid; laying the liquid to form a base; waiting for the base to solidify; laying the liquid iteratively in a pattern to form a plurality of support members protruding from the base, each support member comprising a portion proximate to the base and a portion distal from the base; laying the liquid in a pattern to form a plurality of lateral members interconnecting the distal portions of the support members, forming an open patterned structure above the base that defines an arch covering at least one hollow passageway; and waiting for the liquid to solidify into a completed edge breather.
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