Rapid processing of laminar composite components
US-12180120-B2 · Dec 31, 2024 · US
US9453418B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9453418-B2 |
| Application number | US-201213716930-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 17, 2012 |
| Priority date | Dec 17, 2012 |
| Publication date | Sep 27, 2016 |
| Grant date | Sep 27, 2016 |
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A hollow article includes a metallic hollow article formed from a having a first major surface, an internal cavity with an opening in the first major surface, and a socket around the opening; a cover of composite material received in the socket and covering the opening; and a filler material of foam in the internal cavity.
Opening claim text (preview).
What is claimed is: 1. A hollow airfoil comprising: a metallic article having a first major surface, a second major surface, an internal cavity with an opening in the first major surface, and a first socket around the opening; a second socket formed in the metallic article and disposed around the first socket; a first cover of composite material received in the first socket and covering the opening, wherein the first cover is adhesively bonded to the metallic article; a second composite cover disposed in the second socket and covering the first composite composite cover, wherein the second composite cover is larger than the first composite cover and is adhesively bonded to the second socket and the first composite cover; and a filler material of foam in the internal cavity. 2. The hollow airfoil of claim 1 , wherein the filler material comprises a metallic foam. 3. The hollow airfoil of claim 1 , wherein the filler material comprises a non-metallic foam. 4. The hollow airfoil of claim 1 , wherein the filler material comprises a pourable foam. 5. The hollow airfoil of claim 1 , and further comprising: one or more additional internal cavities between the first and second major surfaces. 6. The hollow airfoil of claim 5 , wherein the one or more additional internal cavities are filled with filler material. 7. The hollow airfoil of claim 6 , wherein all cavities are filled with one or more of: non-metallic foam and metallic foam. 8. The hollow airfoil of claim 1 , further comprising an adhesive bond between the first cover and the filler material disposed within the internal cavity. 9. The hollow airfoil of claim 1 , wherein the first cover and the second cover are bonded to the hollow article with epoxy or urethane. 10. The hollow airfoil of claim 9 , wherein the epoxy or urethane is scrim supported. 11. The hollow airfoil of claim 1 , and further comprising: one or more ribs within the internal cavity. 12. The hollow airfoil of claim 11 , wherein the one or more ribs extend from the first major surface to the second major surface. 13. An airfoil comprising: a hollow metallic airfoil structure with a suction side and a pressure side and one or more internal cavities and an opening on one of the suction side and the pressure side; a first socket formed in the hollow metallic airfoil around the opening; a second socket formed in the hollow metallic airfoil, wherein the second socket is disposed around the first socket; foam material disposed in at least one of the internal cavities; a first composite cover disposed in the first socket and covering the foam material and enclosing the opening, wherein the first cover is adhesively bonded to the first socket; and a second composite cover disposed in the second socket and covering the first composite cover, wherein the second composite cover is larger than the first composite cover and is adhesively bonded to the second socket and the first composite cover. 14. The airfoil of claim 13 , wherein each of the one or more internal cavities is filled with foam. 15. The airfoil of claim 13 , wherein the first composite cover, the hollow metallic airfoil structure and the foam material are adhesively bonded together. 16. A method for making a hollow airfoil, the method comprising: forming the hollow airfoil from a metallic material; forming an opening and at least one cavity in a first major surface of the hollow airfoil; forming a first socket around the opening; forming a second socket around the first socket; filling the at least one cavity with filler material; forming a first composite cover sized and shaped to cover the opening and the first socket; adhesively bonding the first cover to the first socket and the filler material; forming a second composite cover sized and shaped to cover the first cover and the second socket; and adhesively bonding the second cover to the second socket and the second cover. 17. The method of claim 16 , wherein the step of filling the at least one cavity with filler material comprises: injecting a foam material into the cavity.
Porous [e.g., foamed, spongy, cracked, etc.] · CPC title
Selecting composite materials, e.g. blades with reinforcing filaments · CPC title
with permanent bending or reshaping or surface deformation of self sustaining lamina · CPC title
Textile, fabric, cloth, or pile is sandwiched between two distinct layers of material unlike the textile, fabric, cloth, or pile layer · CPC title
Hollow or container type article [e.g., tube, vase, etc.] · CPC title
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