• Title/Summary/Keyword: Oxy-acetylene

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Heated temperature and Range of the Oxy-acetylene Cutting Reinforcing Bar by Simulation and Experiment (시뮬레이션과 실험에 의한 산소절단기 절단시 철근의 수열온도 분포)

  • Kim, Bong-Joo;Kim, Jae-Hun;Cho, Byoung-Hoo
    • Journal of the Korean Society of Hazard Mitigation
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    • v.8 no.2
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    • pp.1-5
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    • 2008
  • The object of this experimental and simulation study is to find out heated temperature and range from the Oxy-acetylene cutting point of reinforcing bars (D10, D13, D16, D19, D22, D25 for each cases of SD3O and SD40) in room temperature ($20{\sim}22^{\circ}C$). This cutting is under the condition that a skilled worker cut one bar per a time. The results are these. 1. The temperature of the point 1 of reinforcing bars cut with Oxy-acetylene cutter is over 700$^{\circ}C$ under 1000$^{\circ}C$, but the temperature of the point 2 of reinforcing bars cut with Oxy-acetylene cutter is under 200$^{\circ}C$ 2. The temperature of the point that is apart 2cm from Oxy-acetylene cutting point is not over 200$^{\circ}C$, so reinforcing bars has not transform to be brittle. The results of simulation for temperatures of the each point apart from Oxy-acetylene cutting point is similar to upper experimental results.

Analysis on Thermochemical Erosion Properties for Thermal Insulation Materials of Graphite Nozzle Throat (흑연 노즐목 내열재의 열화학적 침식 특성 분석)

  • Kim, Young-in;Lee, Soo-yong
    • Journal of Advanced Navigation Technology
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    • v.22 no.2
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    • pp.90-95
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    • 2018
  • In the solid rocket motor (SRM), a thrust of rocket is generated by a nozzle so it is very important device. The nozzle of SRM is a condition of high temperature and high pressure so occurs the erosion by combustion gas. The liquid rocket propulsion systems (LRPSs) cools the nozzle by the fuel and oxidizer but SRM does not cool the nozzle. This paper deal with the development of the oxy-acetylene torch tester and investigate the thermochemical erosion properties for the thermal insulation materials of the graphite rocket nozzle throat through the experiment. The results of experiments are compared with the results of Theoretical model and identify the key factors affecting of erosion. The results is in good agreement with the experimental data.

Ablation Behavior of ZrB2-SiC UHTC Composite under Various Flame Angle Using Oxy-Acetylene Torch (산소-아세틸렌 토치의 조사각이 ZrB2-SiC UHTC 복합체 삭마 특성에 미치는 영향)

  • Seung Yong Lee;Jung Hoon Kong;Jung Hwan Song;Young Il Son;Do Kyung Kim
    • Korean Journal of Materials Research
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    • v.32 no.12
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    • pp.553-559
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    • 2022
  • 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 ℃ 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.

Study on Improvement of Mechanical Property, Oxidation and Erosion Resistance of SiC Matrix Ceramic Composites Reinforced by Hybrid Fabric Composed of SiC and Carbon Fiber (탄화규소섬유와 탄소섬유 하이브리드 직물을 강화재로 한 SiC 매트릭스 세라믹복합재의 기계적물성, 산화 및 삭마 저항성 개선 연구)

  • Yoon, Byungil;Kim, Myeongju;Kim, Jaesung;Kwon, Hyangjoo;Youn, Sungtae;Kim, Jungil
    • Composites Research
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    • v.32 no.3
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    • pp.148-157
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    • 2019
  • In this study, $C_f/SiC$, $SiC_f/SiC$ and $C_f-SiC_f/SiC$ ceramic composites reinforcing carbon fiber, SiC fiber and hybrid fiber were fabricated by hybrid TGCVI and PIP process. After the thermal shock cycle, 3-point bending and Oxy-Acetylene torch test, their mechanical behavior, oxidation and erosion resistance were evaluated. The $C_f/SiC$ composite showed a decrease in mechanical property along with increasing temperature, a pseudo-ductile fracture mode and a large quantity of erosion. The $SiC_f/SiC$ composite exhibited stronger mechanical property and lower erosion rate compared to the $C_f/SiC$, but brittle fracture mode. On the other hand, hybrid type of $C_f-SiC_f/SiC$ composite gave the best mechanical property, more ductile failure mode than the $SiC_f/SiC$, and lower erosion rate than the $C_f/SiC$. During the Oxy-Acetylene torch test, the $SiO_2$ formed by reaction of the SiC matrix with oxygen prevented further oxidation or erosion of the fibers for $C_f-SiC_f/SiC$ and $SiC_f/SiC$ composites particularly. In conclusion, if a hybrid composite with low porosity is prepared, this material is expected to have high applicability as a high temperature thermo-structural composite under high temperature oxidation atmosphere by improving low mechanical property due to the oxidation of $C_f/SiC$ and brittle fracture mode of $SiC_f/SiC$ composite.

Interfacial Microstructure of Diffusion-Bonded W-25Re/Ti/Graphite Joint and Its High-Temperature Stability (확산 접합에 의해 제조된 텅스텐-레늄 합금/티타늄/그래파이트 접합체의 미세구조 및 고온 안정성)

  • Kim, Joo-Hyung;Baek, Chang Yeon;Kim, Dong Seok;Lim, Seong Taek;Kim, Do Kyung
    • Korean Journal of Materials Research
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    • v.26 no.12
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    • pp.751-756
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    • 2016
  • Graphite was diffusion-bonded by hot-pressing to W-25Re alloy using a Ti interlayer. For the joining, a uniaxial pressure of 25 MPa was applied at $1600^{\circ}C$ for 2 hrs in an argon atmosphere with a heating rate of $10^{\circ}C\;min^{-1}$. The interfacial microstructure and elemental distribution of the W-25Re/Ti/Graphite joints were analyzed by scanning electron microscopy (SEM). Hot-pressed joints appeared to form a stable interlayer without any micro-cracking, pores, or defects. To investigate the high-temperature stability of the W-25Re/Ti/Graphite joint, an oxy-acetylene torch test was conducted for 30 seconds with oxygen and acetylene at a 1.3:1 ratio. Cross-sectional analysis of the joint was performed to compare the thickness of the oxide layer and its chemical composition. The thickness of W-25Re changed from 250 to $20{\mu}m$. In the elemental analysis, a high fraction of rhenium was detected at the surface oxidation layer of W-25Re, while the W-25Re matrix was found to maintain the initial weight ratio. Tungsten was first reacted with oxygen at a torch temperature over $2500^{\circ}C$ to form a tungsten oxide layer on the surface of W-25Re. Then, the remaining rhenium was subsequently reacted with oxygen to form rhenium oxide. The interfacial microstructure of the Ti-containing interlayer was stable after the torch test at a temperature over $2500^{\circ}C$.

A Study on the Performance Evaluation of Heat Treatment Furnace Design for Copper Tube Bending (동관 벤딩을 위한 열처리로 설계 및 성능평가에 관한 연구)

  • Park, Dae-kwang;Kim, Jae-yeol;Gao, Jia-Chen
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.15 no.1
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    • pp.136-144
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    • 2016
  • The air-conditioning industry is closely related to types of lifestyles, climate, and products. With the improvement of national income, the pursuit of pleasant living and working environments, and South Korea's four seasons and distinct climatic conditions, demand for air conditioning has increased. In addition, the industry is becoming increasingly precise and cooperative, and the increase in the domestic production of sophisticated air conditioning and continued growth of future industrial cooperation are expected to rapidly rise. Accordingly, the study of air piping systems can improve the productivity and quality of products and cost savings and can achieve vibration reduction. Additionally, using a heat treatment furnace for copper tube annealing treatment reduces the risk of using an oxy-acetylene torch.

Color Enhancement for Cubic Zirconia with Low Temperature Annealing (큐빅지르코니아의 색향상을 위한 저온열처리 공정 연구)

  • Li, Feng;Shen, Yun;Song, Oh-Sung
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.11 no.4
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    • pp.1186-1191
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    • 2010
  • Colored cubic zirconia specimen made by skull melt process were annealed in vacuum at the temperature of $1200^{\circ}C{\sim}1400^{\circ}C$ for 10~60 minutes to enhance the color. All the seven specimen become darker and eventually be black as annealing temperature and time increase. The black samples turned into original colors when we elevated the temperature with oxy-acetylene torch for around 10 minutes in the air. Finally, we could tune the colors of cubic zirconia either anneal in vacuum or the black samples in the air to obtain the proposed colors. Our proposed new process may be appropriate to fabricate the precious synthetic colored cubic zirconia to simulate the natural colored gem quality diamonds.