• 한국군사과학기술학회지
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• 제17권4호
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• pp.413-421
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• 2014

Since the structural temperature of a flight vehicle flying at high speed rises rapidly due to aerodynamic heating, it is necessary for optimum structural design to obtain proper material properties at high temperature by taking into account of its operational environment. For a special alloy, analysis data on strength change due to exposure time to high temperature are very limited, and most of them are for an exposure time longer than 30 minutes for long term operations. In this study, base and weld metal samples of Ti-6Al-4V alloy had been prepared and high temperature tensile tests with induction heating were performed, and then high temperature strength characteristics and strength recovery characteristics through cooling have been analyzed. Pre-tests to determine maximum heating rate were performed, and response characteristics for temperature control were confirmed. As a result, high temperature tensile strength appeared to be lower than that of room temperature, but it was higher than that of high temperature of 30 minite exposure listed in MMPDS. In strength recovery through cooling Ti-6Al-4V alloy has shown higher recovery rate compared with other alloys.

• 한국구조물진단유지관리공학회 논문집
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• 제21권2호
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• pp.53-59
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• 2017

본 연구에서는 고온에 노출된 GFRP 보강근과 고온에 노출된 후 알칼리용액에 노출된 보강근의 단면을 현미경을 통해 관찰하고 발생된 손상의 특징을 고찰하였다. 또한, 각 시험체에 발생한 레진 균열과 공극에 대한 정량적 분석을 실시하였다. 알칼리로 인한 손상은 주로 표면에 집중되며 레진균열과 작은 공극을 발생시키는 것으로 확인되었다. 고온노출에 의한 손상은 레진균열과 공극을 발생시키는 것은 알칼리와 동일하지만 전단면에서 발생하며, 공극의 크기가 훨씬 크다. 또한 정량분석 결과, 동일한 알칼리 용액 노출조건에도 불구하고, $200^{\circ}C$ 이상의 고온에 노출된 시편에서 발견된 레진 균열과 공극이 고온노출이력이 전혀 없는 보강근에서 발견된 것 보다 1.5 및 1.4배 큰 것으로 확인되었다. 그러므로 동일한 알칼리 노출 조건이라 할지라도 $200^{\circ}C$ 이상의 고온에 노출된 보강근은 고온노출이력이 없는 보강근에 비하여 레진의 열화가 가속화 될 가능성이 있음을 알 수 있다.

• 대한토목학회논문집
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• 제35권1호
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• pp.77-84
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• 2015

고온에 노출된 GFRP 보강근의 인장실험을 수행하였다. 본 실험을 위한 고온노출조건은 $200^{\circ}C$ 이하의 온도에 3분간 노출하는 것으로 하였다. 이러한 조건은 다른 연구자들의 시험에서 적용한 고온노출조건과 비교하여 경미한 고온노출조건이다. 고온에서와 고온노출 후 GFRP 보강근의 인장강도와 탄성계수를 비교하였다. 실험결과, 고온에서 GFRP 보강근의 인장성능이 감소하는 것으로 나타났으나, 고온노출 후 보강근의 인장성능은 거의 고온노출전의 수준으로 회복되는 것으로 나타났다. 이와 같은 결과는 화재로 손상 받은 GFRP 보강 콘크리트 구조물의 평가를 위하여 중요한 자료가 된다.

• 한국직업건강간호학회지
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• 제31권2호
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• pp.95-103
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• 2022

Purpose: This study aims to identify general, workplace, and health-related characteristics of outdoor workers exposed to high temperatures, and to compare the risk of disease according to outdoor high temperature exposure. Methods: This secondary analysis study used the 5th Korean Working Conditions Survey (2017) to identify 4,915 outdoor workers exposed to high temperatures. Results: Outdoor workers exposed to high temperatures were mostly male, elderly, less educated, and daily contract workers. Most of them were engaged in agriculture, forestry and fishing, and construction industries. About 40~50% of them complained of musculoskeletal pain and overall fatigue. The results showed that high temperature exposure increased the risk of illness (hearing problem, skin problem, backache, muscular pains in upper and lower limbs, headache/eyestrain, injuries, depression, and overall fatigue) among workers. Conclusion: High temperature exposure might increase the risk of illness among workers. The results of this study demonstrated that the outdoor workers should be protected from high temperatures.

• 한국주조공학회지
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• 제37권5호
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• pp.139-147
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• 2017

Microstructural evolution of cast Hastelloy X during thermal exposure has been investigated. OM, SEM, and TEM microscopy were carried out on the as-cast, the standard heat treated, and the thermally exposed conditions. Tensile tests were also conducted to understand the effect of microstructural evolution on the degradation of tensile properties. Coarse $M_6C$ and fine $M_{23}C_6$ carbides were found in as-cast Hastelloy X with fine carbides on sub-boundary. Some of $M_{23}C_6$ carbide dissolved into the matrix during solution heat treatment and dislocation network formed at the interface between the carbide and the matrix due to the misfit strain. There was no significant microstructural difference between the exposed specimens at $400^{\circ}C$ and the solution heat treated specimen. A large amount of $M_{23}C_6$ carbides precipitated along and near grain boundaries and sub-boundaries after exposure at $650^{\circ}C$. Exposure at $870^{\circ}C$ of the alloy caused precipitation of $M_6C$ and ${\mu}$. The strength increased and the elongation decreased by thermal exposure at $650^{\circ}C$ and $870^{\circ}C$ because carbides interfere with the movement of the dislocation. It was found that the precipitation of carbide gave significant effects on the tensile properties of Hastelloy X.

• 항공우주시스템공학회지
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• 제2권2호
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• pp.42-45
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• 2008

Under the non-operating exposure condition in the hot area, the T-50 cockpit temperature is expected over the requirement according to T-50 environmental criteria. So it is necessary to protect the cockpit from the high temperature condition during the non-operating exposure because the high temperature of the cockpit may result in the cockpit equipment malfunction. In this study, the transparency coating is selected as the method for protecting the cockpit from the high temperature exposure and analyzed the effect on the cockpit heat load attenuation. Some kinds of cockpit coating were reviewed and selected and the analysis was performed about the effect before and after coating application under 1% hot day condition based on the T-50 FSD hot soaking test data. The result of analysis show transparency coating is so effective to attenuate the heat load of T-50 cockpit.

• 한국주조공학회지
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• 제36권5호
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• pp.159-166
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• 2016

The microstructural evolution of a cast Ni base superalloy, IN738LC, has been investigated after long term exposure at several temperatures. Most of the fine secondary ${\gamma}^{\prime}$ particles resolved after 2000 hour exposure at $816^{\circ}C$. At higher temperatures of $871^{\circ}C$ and $927^{\circ}C$, secondary ${\gamma}^{\prime}$ resolved after 1000 hours of exposure, and cuboidal primary ${\gamma}^{\prime}$ grew with exposure time. During the thermal exposure, ${\sigma}$ phase formed at all tested temperatures, and ${\eta}$ phase was observed around interdendritic regions due to carbide degeneration. The influence of microstructural evolution during thermal exposure on the mechanical properties has been analyzed. The effects of ${\gamma}^{\prime}$ particle growth are more pronounced on the high temperature creep properties than on the room temperature tensile properties.

• 콘크리트학회논문집
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• 제25권1호
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• pp.45-51
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• 2013

고온에 노출된 GFRP와 CFRP 보강근의 단지간보 실험을 통해 계면전단강도를 측정하였다. 1차 실험으로서, 노출시간과 온도를 변수로 하였으며, 적용된 고온 조건하에서 강도의 변화를 고찰하였으다. 1차 실험의 결과로부터 두가지 보강근에 대하여 임계온도가 $270^{\circ}C$로 동일한 것을 확인하였다. 이 연구에서 임계온도는 상온에서의 계면전단강도의 50%의 손실을 발생시키는 온도로 정의하였다. 계면전단강도에 대한 임계온도는 섬유의 종류가 아닌 레진이 성능에 지배된다는 것이다. 2차 실험에서는 임계온도하에서 0.25시간의 간격으로 노출시간에 대한 영향을 고찰하였다. 모든 실험 결과로부터, 노출시간의 영향은 노출온도에 비하여 그 영향이 크진 않지만 무시할 정도는 아닌 것으로 나타났다. 더욱이, 그 영향은 임계온도하에서 매우 중대함을 확인하였다.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2003년도 가을 학술발표회 논문집
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• pp.625-628
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• 2003

This paper presents the behaviors of reinforced concrete columns under high temperature. When columns are exposed high temperature, temperature distribution of a section becomes nonlinear and it is calculated by using finite difference method(F.D.M). The interaction curves show the strength of columns at various exposure times. The strength of columns decreases according to the increase of the exposure time and the decrease of concrete cover.

• 한국재료학회지
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• 제23권9호
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• pp.531-536
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• 2013

This paper investigates the effect of prolonged high temperature exposure on concentric laminated $Al_2O_3-ZrO_2$ composites. An ultrafine scale microstructure with a cellular 7 layer concentric lamination with unidirectional alignment was fabricated by a multi-pass extrusion method. Each laminate in the microstructure was $2-3{\mu}m$ thick. An alternate lamina was composed of 75%$Al_2O_3$-(25%m-$ZrO_2$) and t-$ZrO_2$ ceramics. The composite was sintered at $1500^{\circ}C$ and subjected to $1450^{\circ}C$ temperature for 24 hours to 72 hours. We investigated the effect of long time high temperature exposure on the generation of residual stress and grain growth and their effect on the overall stability of the composites. The residual stress development and its subsequent effect on the microstructure with the edge cracking behavior mechanism were investigated. The residual stress in the concentric laminated microstructure causes extensive micro cracks in the t-$ZrO_2$ layer, despite the very thin laminate thickness. The material properties like Vickers hardness and fracture toughness were measured and evaluated along with the microstructure of the composites with prolonged high temperature exposure.