Tantalum carbide-covered carbon material and process for producing the same
A technology of tantalum carbide and carbon materials, applied in the direction of gaseous chemical plating, metal material coating process, coating, etc., can solve the problems of reduced softness, easy cracks, and shortened life of carbon materials, so as to achieve inhibition of release, Effect of reducing corrosion, reducing cracks and peeling
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Embodiment 1~3
[0107] Set the coefficient of thermal expansion to 7.8×10 -6 / K, 1000 ℃ base gas release pressure is 10 - 6 A graphite substrate with a diameter of 66 mm and a thickness of 10 mm in Pa / g and an ash content of 2 ppm was subjected to the above-mentioned halogen treatment, and then a tantalum carbide coating film was formed on the carbon substrate under the CVD conditions in Table 1 below. At this time, the composition ratio of C / Ta of the coating film passes C 3 h 8 The flow rate is adjusted to 1.0~1.2. Using the CVD conditions shown in Table 1, the film thickness was changed to 21, 34, 44 μm by changing the reaction time to 11, 18, 25 hours. Then, heat treatment was further performed at 2000° C. for 10 hours in a hydrogen atmosphere to further improve the crystallinity of the coating film 3 . The X-ray diffraction result of embodiment 1~3 is as Figure 15 ~ Figure 17 shown. In X-ray diffraction, the diffraction lines of the (220) plane were mainly confirmed, and the diff...
Embodiment 4~8
[0114] On the same carbon substrate 1 as used in Examples 1 to 3, a tantalum carbide coating film 3 was formed by a CVD method. The CVD conditions are as follows: the temperature is fixed at 850°C, the pressure is fixed at 1330Pa, and the C 3 h 8 and TaCl 5 The flow rate changes the growth rate of tantalum carbide in the range of 1-30μm / hr. In Examples 4 to 6, after the coating film 3 was formed, heat treatment was performed at 2000° C. for 10 hours in a hydrogen atmosphere. The obtained crystal structure of the coating film 3 was detected by X-ray diffraction. As a result, the intensity ratio of the (220) plane diffraction line was the strongest, which was 4 times or more the intensity of the second strongest diffraction line. As shown in Table 3, the half value width of the diffraction line of the (220) plane of the coating film 3 is in the range of 0.11° to 0.14°. It is preferable that such a coating film does not cause cracks or peeling before the thermal shock resista...
Embodiment 9~18
[0119] Carbon materials 100 were produced using various graphite substrates 1 having the properties shown in Table 4. The above-mentioned halogen treatment was performed on graphite substrates having a diameter of 60 mm and a thickness of 10 mm having various coefficients of thermal expansion (CTE) shown in Table 4, so that the ash content of the graphite substrate was 10 ppm or less. However, in Example 18, this halogen treatment was omitted, and the ash content of the graphite substrate 1 was 16 ppm. A tantalum carbide coating film 3 (thickness: 43 μm) was formed on the substrate under the same conditions as in Examples 1 to 3. The composition ratio of C / Ta of coating film 3 is determined by C 3 h 8 The flow rate is adjusted to 1.0-1.2. After the coating film 3 was formed, heat treatment was performed at 2000° C. for 10 hours in a hydrogen atmosphere. In the coating films of Examples 9 to 18, the (220) planes all show the strongest diffraction intensity, which is 4 times...
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