Methods of forming composite material films
US-10103378-B2 · Oct 16, 2018 · US
US9770841B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9770841-B2 |
| Application number | US-201514717253-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 20, 2015 |
| Priority date | May 30, 2014 |
| Publication date | Sep 26, 2017 |
| Grant date | Sep 26, 2017 |
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Embodiments of the present disclosure relate to a hot press and methods of using the hot press. In an embodiment, the hot press can include a pressing element including a flared body. In another embodiment, the hot press can include a compression surface. The compression surface can include a first layer including a monocrystalline material and a second layer including a polycrystalline material, wherein the monocrystalline material and the polycrystalline material include a same primary compound. In a further embodiment, a sample including more than one layer of ceramic oxide material can be hot pressed without a die.
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What is claimed is: 1. A hot press, comprising: a chamber with a heating element, wherein the chamber includes an upper wall; and first pressing element including a first flared body positioned within the chamber and adjacent the upper wall of the chamber, wherein the first flared body includes an expanded major surface facing away from the upper wall of the chamber. 2. The hot press of claim 1 , wherein the hot press does not include a die or a mold. 3. The hot press of claim 1 , wherein the first pressing element includes a silicon carbide, an aluminum oxide, a zirconia, or any combination thereof. 4. The hot press of claim 1 , wherein the hot press comprises a first compression surface comprising a first layer including a monocrystalline material and a second layer including a polycrystalline material, wherein the first compression surface is adjacent the expanded major surface, and wherein the monocrystalline material and polycrystalline material include a same primary compound. 5. The hot press of claim 4 , wherein the monocrystalline material includes sapphire. 6. The hot press of claim 4 , wherein the polycrystalline material includes an aluminum oxide. 7. The hot press of claim 4 , wherein the hot press comprises a second compression surface comprising a third layer including a monocrystalline material and a fourth layer including a polycrystalline material, wherein the monocrystalline material and polycrystalline material include a same primary compound. 8. The hot press of claim 7 , wherein the first compression surface and the second compression surface are aligned in an axial direction. 9. The hot press of claim 1 , wherein the hot press comprises a second pressing element including a second flared body. 10. A hot press, comprising: a chamber with a heating element; a first push rod including a silicon carbide; and a first pressing element positioned within the chamber and adjacent the first push rod. 11. The hot press of claim 10 , wherein the hot press does not include a die or a mold. 12. The hot press of claim 10 , further comprising a first compression surface including a silicon carbide, an aluminum oxide, a zirconia, or any combination thereof, wherein the first compression surface is adjacent the first pressing element. 13. The hot press of claim 10 , wherein the hot press comprises a second push rod including a silicon carbide and aligned in an axial direction with the first push rod. 14. The hot press of claim 10 , comprising a pressing unit including a plurality of compression surfaces aligned in an axial direction. 15. The hot press of claim 14 , comprising a plurality of the pressing units arranged in rows and columns. 16. A method of manufacturing a ceramic product including a plurality of layers, comprising: placing a sample on a compression surface in a hot press; and pressing the sample to form the ceramic product including the plurality of layers, wherein during pressing, the hot press does not include a die. 17. The method of claim 16 , wherein the ceramic product including the plurality of layers is at least a part of a fuel cell or a multilayer ceramic structure. 18. The method of claim 16 , comprising placing a spacer between the compression surface and the sample. 19. The method of claim 18 , wherein the spacer includes sapphire, an aluminum oxide, a silicon carbide, a zirconia, or any combination thereof. 20. The method of claim 16 , comprising exposing the sample to a thermal gradient so that a temperature difference between an edge of the sample and a center of the sample is not greater than 25° C.
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