Method of coating surface of inorganic powder particles with silicon-carbon composite and inorganic powder particles coated by the same
US-9221025-B2 · Dec 29, 2015 · US
US10106889B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10106889-B2 |
| Application number | US-201514937669-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 10, 2015 |
| Priority date | Nov 11, 2014 |
| Publication date | Oct 23, 2018 |
| Grant date | Oct 23, 2018 |
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Waveguides that include a top cladding layer; a bottom cladding layer; and a core layer positioned between the top cladding layer and the bottom cladding layer, the core layer including a material having a refractive index of not less than 2.1, for example amorphous hydrogenated silicon carbide (SiC:H), or bismuth titanate. Methods of forming core layers of waveguides are also disclosed.
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What is claimed is: 1. A waveguide comprising: a top cladding layer; a bottom cladding layer; and a core layer positioned between the top cladding layer and the bottom cladding layer, the core layer comprising amorphous hydrogenated silicon carbide (SiC:H) having a carbon content of not greater than 50% based on the total amount of carbon and silicon, or bismuth titanate and having a thickness from 75 nanometers (nm) to 150 nm. 2. The waveguide according to claim 1 , wherein the core layer comprises amorphous hydrogenated silicon carbide (SiC:H). 3. The waveguide according to claim 2 , wherein the core layer has a refractive inded of not less than 2.3. 4. The waveguide according to claim 2 , wherein the carbon content of the amorphous hydrogenated silicon carbide (SiC:H) is not greater than 46% based on the total amount of carbon and silicon. 5. The waveguide according to claim 2 , wherein the carbon content of the amorphous hydrogenated silicon carbide (SiC:H) is not greater than 38% based on the total amount of carbon and silicon. 6. The waveguide according to claim 1 , wherein the core layer comprises bismuth titanate. 7. The waveguide according to claim 1 , wherein the top cladding layer, the bottom cladding layer, or both independently comprise SiO 2 , MgF 2 , Al 2 O 3 , porous silica, or combinations thereof. 8. The waveguide according to claim 1 , wherein the core layer has a thickness from 80 nanometers (nm) to 100 nm. 9. An apparatus comprising: a light source; a near field transducer (NFT); and a waveguide, the waveguide comprising: a top cladding layer; a bottom cladding layer; and a core layer positioned between the top cladding layer and the bottom cladding layer, the core layer comprising amorphous hydrogenated silicon carbide (SiC:H), or bismuth titanate and having a thickness from 75 nanometers (nm) to 150 nm, wherein the waveguide is configured to receive light from the light source and transmit it to the NFT. 10. The apparatus according to claim 9 , wherein the core layer comprises amorphous hydrogenated silicon carbide (SiC:H). 11. The apparatus according to claim 9 , wherein the carbon content of the amorphous hydrogenated silicon carbide (SiC:H) is not greater than 50% based on the total amount of carbon and silicon. 12. The apparatus according to claim 9 , wherein the carbon content of the amorphous hydrogenated silicon carbide (SiC:H) is not greater than 38% based on the total amount of carbon and silicon. 13. The apparatus according to claim 9 , wherein the core layer comprises bismuth titanate. 14. The apparatus according to claim 9 , wherein the core layer has a thickness from 80 nm to 100 nm. 15. A method of forming a waveguide, the method comprising: depositing a layer of hydrogenated amorphous silicon carbide (SiC:H); and annealing the deposited layer of hydrogenated amorphous silicon carbide (SiC:H), wherein the annealed hydrogenated amorphous silicon carbide (SiC:H) has a refractive index of not less than about 2.3 at about 830 nm. 16. The method according to claim 15 , wherein the step of depositing the layer hydrogenated amorphous silicon carbide (SiC:H) comprises chemical vapor deposition (CVD). 17. The method according to claim 16 , wherein the precursor gas for the carbon source comprises methane (CH 4 ), propene (C 3 H 6 ), propane (C 3 H 8 ), hexane (C 6 H 14 ), xylene (C 8 H 10 ), or combinations thereof; and the precursor gas for the silicon source comprises silane (SiH 4 ), disilane (Si 2 H 6 ), tetrachlorosilane (SiCl 4 ), or combinations thereof. 18. The method according to claim 15 , wherein the annealing occurs at a temperature of not less than about 220° C. 19. The method according to claim 16 , wherein the CVD comprises use of a dilution/carrying gas that comprises argon (Ar), helium (He), or combinations thereof. 20. The method according to claim 15 , wherein the hydrogenated amorphous silicon carbide (SiC:H) has a refractive index of not less than about 2.5 at about 830 nm.
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