To test a flameproof enclosure for the safety certificate, a reference pressure of explosion needs to be determined. However, the explosion pressure may be changed according to relative humidity of explosive gases. Therefore, the guideline on relative humidity should be recommended for measuring the explosion pressure for accurate and reproducible testings. This study examined the relationship of explosion pressure with relative humidity of hydrogen (31 vol %)-air and acetylene (14 vol %)-air mixture gases. The explosion pressures were measured by increasing the relative humidity of the gases by 10 % from dry state to 80 % in a cylindrical explosion enclosure of 2.3 L. on ambient temperature and atmospheric pressure (1 atm). The maximum explosive pressures were remained almost constant until the relative humidity reached 10 % for the hydrogen-air mixture and 20 % for the acetylene-air mixture. However, the maximum explosive pressures linearly decreased as the relative humidity increased. Based on the results of the study, it would be recommended to use 10 % relative humidity for the hydrogen-air mixture and 20 % for the acetylene-air mixture as the critical value in testing a flameproof enclosure.

In this work, the ablation behavior of monolith ZrB2-30 vol%SiC (Z30S) composites were studied under various oxy-acetylene flame angles. Typical oxidized microstructures (SiO2/SiC-depleted/ZrB2-SiC) were observed when the flame to Z30S was arranged vertically. However, formation of the outmost glassy SiO2 layer was hindered when the Z30S was tilted. The SiC-depleted region was fully exposed to air with reduced thickness when highly tilted. Traces of the ablated and island type SiO2 were observed at intermediate flame angles, which clearly verified the effect of flame angle on the ablation of the SiO2 layer. Furthermore, the observed maximum surface temperature of the Z30S gradually increased up to 2,200 °C proving that surface amorphous silica was continuously removed while monoclinic ZrO2 phase began to be exposed. A proposed ablation mechanism with respect to flame angles is discussed. This observation is expected to contribute to the design of complex-shaped UHTC applications for hypersonic vehicles and re-entry projectiles.

본 연구에서는 메탄 대향류 확산 화염내 탄소나노튜브의 합성에 대하여 실험 및 수치적 연구를 수행하였다. 아세틸렌을 일정비율로 메탄에 혼합하여 연료 가스로 사용하였으며, 탄소나노튜브의 합성을 위한 촉매로서 페로센이 이용되었다. 주요 인자로는 메탄 연료에 대한 아세틸렌의 혼합비율이며, 2 %, 6 %, 10 %로 혼합하였다. 탄소나노튜브를 채취한 그리드 위의 탄소나노튜브 합성 특성은 SEM 이미지로 분석되었다. 수치해석에서 화학반응 메카니즘으로는 GRI-Mech 3.0 이 적용되었다. 수치결과로는 아세틸렌 혼합 비율이 증가할수록 화염 온도도 증가하며 CO 몰분율도 증가하는 것을 알 수 있다. 실험결과로는 2% 아세틸렌 혼합 화염이 6 % 및 10 % 혼합 화염과 비교해 탄소나노튜브 합성이 잘 이루어졌음을 알 수 있었다. 이것은 6 % 및 10 % 아세틸렌 혼합화염의 경우 과도한 카본 소스의 생성이 발생해 오히려 화염 내 카본소스가 촉매입자로의 공급을 방해하기 때문이라 생각한다. 이 결과로부터 양호한 질의 탄소나노튜브 생성을 위해서는 적정한 양의 카본소스가 생성되어야 한다는 것을 알 수 있었다.

Multi-walled carbon nanotubes (CNTs) were prepared by thermal chemical vapor deposition (CVD) and microwave plasma chemical vapor deposition (MPCVD) using various combination of binary catalysts with four transition metals such as Fe, Co, Cu, and Ni. In the preparation of CNTs from acetylene precursor by thermal CVD, the CNTs with very high yield of 43.6 % was produced over Fe-Co/Al2O3. The highest yield of CNTs was obtained with the catalyst reduced for 3 hr and the yield was decreased with increasing reduction time to 5 hr, due to the formation of FeAl2O4 metal-aluminate. On the other hand, the CNTs prepared by acethylene plasma CVD had more straight, smaller diameter, and larger aspect ratio(L/D) than those prepared by thermal CVD, although their yield had lower value of 27.7%. The degree of graphitization of CNTs measured by Id/Ig value and thermal degradation temperature were 1.04 and 602℃, respectively.