Method for producing a roll-clad aluminum workpiece, roll-clad aluminum workpiece, and use therefor
US-2015375345-A1 · Dec 31, 2015 · US
US9688054B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9688054-B2 |
| Application number | US-201414520991-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 22, 2014 |
| Priority date | Dec 31, 2013 |
| Publication date | Jun 27, 2017 |
| Grant date | Jun 27, 2017 |
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Disclosed is a multi-layered composite panel. The multi-layered composite panel comprises at least two sheets of thin plates with continuous waveform patterns having the same pitch and different heights in one direction are overlapped. In the multi-layered composite panel, an air layer is formed between the overlapping thin plates, orthogonal pressing portions, which divide the waveform patterns on the top and the bottom of the thin plates into the unit of triangle-patterned cell by being pressed orthogonally to cross each other on the top and the bottom of the thin plates overlapping in the orthogonal direction crossing the direction of the waveform patterns, are formed and an undercut portion is formed by pressing the centers of both sides connecting a groove and a ridge of each cell on the top and the bottom of the thin plates with opposite orthogonal pressing portions.
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What is claimed is: 1. A multi-layered composite panel, comprising at least two sheets of thin plates, wherein the two sheet of thin plates include continuous waveform patterns having the same pitch and different heights in one direction and are overlapped, and an air layer is formed between the overlapping thin plates; orthogonal pressing portions, which divide the waveform patterns on the top and the bottom of the thin plates into the unit of triangle-patterned cell by being pressed orthogonally to cross each other on the top and the bottom of the thin plates overlapping in the orthogonal direction crossing the direction of the waveform patterns, are formed; and an undercut portion is formed by pressing the centers of both sides connecting a groove and a ridge of each cell on the top and the bottom of the thin plates with opposite orthogonal pressing portions. 2. The multi-layered composite panel of claim 1 , wherein the air layer is formed to be closed in the unit of triangle-patterned cell between the overlapping thin plates by the orthogonal pressing portions between the ridge and the ridge and between the groove and the groove. 3. The multi-layered composite panel of claim 1 , wherein the overlapping thin plates are a top plate and a bottom plate, which are made of aluminum. 4. The multi-layered composite panel of claim 1 , wherein the overlapping thin plates are a top plate and a bottom plate which have about the same thickness. 5. The multi-layered composite panel of claim 1 , wherein the overlapping thin plates are a top plate and a bottom plate which have different thicknesses. 6. The multi-layered composite panel of claim 1 , wherein the waveform pattern is a sine waveform pattern continuous in one direction. 7. The multi-layered composite panel of any one of claim 1 , wherein the orthogonal pressing portions are formed by pressing, in the zigzag shape on the top and the bottom of the overlapping thin plates. 8. The multi-layered composite panel of claim 1 , wherein at the orthogonal pressing portions, the thin plates are in contact with each other. 9. The multi-layered composite panel of a claim 1 , wherein the cell unit includes a triangle-patterned closed air layer formed between the overlapping thin plates by the orthogonal pressing portions between the ridge and the ridge and between the groove and the groove. 10. The multi-layered composite panel of claim 1 , wherein the crossing orthogonal directions have an acute angle and an obtuse angle with respect to the direction of the waveform patterns. 11. A heat protector of a vehicle manufactured using the multi-layered composite panel of claim 1 . 12. A method of manufacturing a heat protector of a vehicle, comprising: press-forming to an external shape of the heat protector in a pressing process using the multi-layered composite panel of claim 1 . 13. A multi-layered composite panel, comprising: a uniform air layer formed between a top plate and a bottom plate, which are aluminum thin plates with continuous waveform patterns having the same pitch and different heights and overlap each other; orthogonal pressing portions, which divide the waveform patterns on the top plate and the bottom plate into the unit of triangle-patterned cell by being pressed orthogonally to cross each other on the top of the top plate and the bottom of the bottom plate overlapping in the orthogonal direction crossing the direction of the waveform patterns, are formed; and an undercut portion is formed by pressing the centers of both sides connecting a groove and a ridge of each triangle-patterned cell on the overlapping top and bottom plates with opposite orthogonal pressing portions. 14. The multi-layered composite panel of claim 13 , wherein the air layer is formed to be closed in the unit of triangle-patterned cell between the ridges and between the grooves of the overlapping top and bottom plates by the orthogonal pressing portions. 15. The multi-layered composite panel of claim 13 , wherein the top plate and the bottom plate are about the same in thickness. 16. The multi-layered composite panel of claim 13 , wherein the top plate and the bottom plate are different in thickness. 17. The multi-layered composite panel of claim 13 , wherein the waveform pattern is a sine waveform pattern continuous in one direction. 18. The multi-layered composite panel of claim 13 , wherein at the orthogonal pressing portions, the top plate and the bottom plate are in contact with each other. 19. The multi-layered composite panel of claim 14 , wherein the cell unit includes a triangle-patterned closed air layer formed between the ridges and between the grooves of the overlapping top and bottom plates, by the orthogonal pressing portions.
comprising aluminium or copper {(B32B15/016 and B32B15/017 take precedence)} · CPC title
Layered products having a non-planar shape · CPC title
characterised by features of form at particular places, e.g. in edge regions {(non-uniform thickness B32B3/263)} · CPC title
having particular thermal properties · CPC title
Vehicles · CPC title
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