Carbon composite composition and carbon heater manufactured using the same
US-2018327323-A1 · Nov 15, 2018 · US
US2018343704A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2018343704-A1 |
| Application number | US-201815986107-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 22, 2018 |
| Priority date | May 26, 2017 |
| Publication date | Nov 29, 2018 |
| Grant date | — |
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A carbon heating element and a method for manufacturing a carbon heating element are provided. The carbon heating element may efficiently dissipate heat and prevent disconnection or destruction of a heating element to prolong a lifespan thereof without generating a spark and plasma under a high voltage. The carbon heating element may include carbon (C) and silicon carbide (SiC), and the carbon heating element may have a thermal conductivity of 1.6 W/m·K or more.
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What is claimed is: 1 . A heating element for a carbon heater, the heating element comprising: carbon (C); and silicon carbide (SiC), wherein the heating element has a thermal conductivity of 1.6 W/m·K or more. 2 . The heating element according to claim 1 , wherein the SiC includes β-SiC and α-SiC. 3 . The heating element according to claim 1 , wherein a degree of crystallization of the SiC in the heating element has a full width at half maximum (FWHM) value of 0.14 as a result of analyzing an X-ray diffraction. 4 . The heating element according to claim 1 , wherein the heating element includes silicon oxide (SiO 2 ). 5 . The heating element according to claim 4 , wherein a total amount of oxygen (O 2 ) in the heating element is 2 wt. % or less. 6 . The heating element according to claim 1 , wherein a specific resistance of the heating element is (11˜16)*10 −2 Ωcm. 7 . The heating element according to claim 1 , wherein the heating element is solid. 8 . The heating element according to claim 1 , wherein the heating element is hollow. 9 . A method for manufacturing a carbon heating element, the method comprising: a process of mixing a heating element composition; a thermal extrusion process; a stabilization heat treatment process; and a carbonization heat treatment process. 10 . The method according to claim 9 , wherein the heating element composition includes: a base material that determines a specific resistance of a heating element; a specific resistance controlling agent that controls a specific resistance of the heating element; a lubricant; and a binder for mechanical coupling between inorganic powders. 11 . The method according to claim 9 , wherein the base material is silicon carbide (SiC). 12 . The method according to claim 10 , wherein the specific resistance controlling agent is SiO 2 . 13 . The method according to claim 10 , wherein the lubricant is graphite. 14 . The method according to claim 10 , wherein the binder is a novolac resin. 15 . The method according to claim 9 , wherein the extrusion process is performed at a speed of about 60 rpm at 100 to 200° C. 16 . The method according to claim 9 , wherein the stabilization heat treatment process is performed at 270 to 320° C. for 10 minutes to 2 hours. 17 . The method according to claim 9 , wherein the carbonization heat treatment process includes a first carbonization heat treatment process for out-gassing at 600 to 1,000° C. for 10 minutes to 2 hours. 18 . The method according to claim 9 , wherein the carbonization heat treatment process includes a second carbonization heat treatment process. 19 . The method according to claim 18 , the second carbonization heat treatment process is performed at 1,200 to 1,400° C. for 10 minutes to 4 hours. 20 . The method according to claim 18 , wherein the carbonization heat treatment process further includes a third carbonization heat treatment process performed at 1,500 to 1,700° C. for 10 minutes to 4 hours. 21 . A carbon heating element manufactured using the method of claim 9 .
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