• Journal of Advanced Marine Engineering and Technology
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• 제25권6호
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• pp.1228-1236
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• 2001

In this study, CT specimens were prepared from ASTH A5l6 steel which was used for pressure vessel plates for moderate and lower temperature service. And we got the fellowing characteristics from fatigue crack growth test carried out in the environment of room and low temperature at $25^{\circ}C$ , $-30^{\circ}C$, $-60^{\circ}C$, $-80^{\circ}C$, $-100^{\circ}C$ and $-120^{\circ}C$ and in the range of stress ratio of 0.1, 0.3 by means of opening mode displacement. At the constant stress ratio, the Threshold stress intensity factor range ΔAKth in the early stage of fatigue crack growth (Region I) and stress intensity factor range $\DeltaK$ in the stable of fatigue crack growth (Region II) was increased in proportion to descend temperature. It assumed that the fatigue resistance characteristics and fracture strength at low temperature is considerable higher than that of room temperature in the early stage and stable of fatigue crack growth region. The straight line slope relation of logarithm da/dN-$\Delta$K in Region II that is, the fatigue clack growth exponent m increased with descending temperature at the constant stress ratio. It assumed that the fatigue crack growth rate da/dN is rapid in proportion to descend temperature in Region II and the cryogenic-brittleness greatly affect a material with decreasing temperature.

• 한국해양공학회지
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• 제14권3호
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• pp.78-83
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• 2000

In this study, CT specimens were prepared from AST SA516 Gr. 70 which was used for pressure vessel plates for room and low temperature service. And we got the following characteristics from fatigue crack growth test carried out in the environment of room and low temperature at 25$^{\circ}C $, -60$^{\circ}C $, -80$^{\circ}C $ and -100$^{\circ}C $ and in the range of stress ratio of 0.05, 0.3 by means of opening mode displacement. At the constant stress ratio, the threshold stress intensity factor range ${\delta} K_{th}$ in the early stage of fatigue crack growth (Region I) and stress intensity factor range $\delta $K in the stable of fatigue crack growth (Region II) were increased in proportion to descending temperature. It was assumed that the fatigue resistance characteristics and fracture strength at low temperature is considerable higher than that of room temperature in the early stage and stable of fatigue crack growth region. The straight line slope relation of logarithm da/dN -$\delta $K in Region II, that is, the fatigue crack growth exponent m increased with descending temperature at the constant stress ratio. It was assumed that the fatigue crack growth rate da/dN is rapid in proportion to descending temperature in Region II and the cryogenic-brittleness greatly affect a material with decreasing temperature.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2001년도 춘계학술대회 논문집
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• pp.326-331
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• 2001

In this study. CT specimens were prepared from ASME SA5l6 which was used for pressure vessel plates for room and low temperature service. And we got the following characteristics from fatigue crack growth test carried out in the environment of room and low temperature at $25^{\circ}C$, -3$0^{\circ}C$, -6$0^{\circ}C$, -8$0^{\circ}C$, -10$0^{\circ}C$ and -12$0^{\circ}C$ in the range of stress ratio of 0.1 by means of opening mode displacement. At the constant stress ratio, the threshold stress intensity factor range ΔKsub/th/ in the early stage of fatigue crack growth ( Region I) and stress intensity factor range ΔK in the stable of fatigue crack growth ( Region II) was increased in proportion to descend temperature. It assumed that the fatigue resistance characteristics and fracture strength at low temperature is considerable higher than that of room temperature in the early stage and stable of fatigue crack growth region. The straight line slope relation of logarithm da.dN -ΔK in RegionII, that is, the fatigue crack growth exponent m increased with descending temperature at the constant stress ratio. It assumed that the fatigue crack growth rate da/dN is rapid in proportion to descend temperature in Region II and the cryogenic-brittleness greatly affect a material with decreasing temperature.

• Journal of Advanced Marine Engineering and Technology
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• 제41권4호
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• pp.345-352
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• 2017

본 연구에서는 액화천연가스(Liquefied natural gas, LNG) 운반선 화물창 손상으로 인한 극저온 LNG 누출 및 하중 작용 시 화물창의 초저온 보냉재를 구성하고 있는 고분자 폼(Polymer foam) 소재의 성능을 관찰하고자 하였다. LNG와 맞닿아 있는 LNG 운반선 1차 방벽은 유체 충격하중이나 오랜 시간 동안의 LNG 적재/하역으로 인해 손상이 누적 되면 누출로 이어지게 된다. 극저온 유체의 누출은 다공성 밀폐 셀 구조인 고분자 폼 내부에 영향을 끼쳐 작용 하중에 대한 거동변화를 야기한다. 본 연구에서는 단열재(Insulation)로 사용되는 고분자 소재인 폴리이소시아누레이트 폼(Polyisocyanurate foam, PIF) 시험편의 기계적 성능에 대한 평가를 수행하였다. 시험편에 극저온 액체를 함침시켜 압축실험을 진행함으로써 저온 취성(Cold brittleness)으로 인한 성능 변화와 함께 극저온 유체의 함침 영향에 대해 정량적으로 비교분석 하였다.

• 한국해양공학회지
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• 제15권3호
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• pp.100-106
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• 2001

In this study, CT specimens were prepared from Pressure Vessel Steel which was used for pressure vessel plates for room and low temperature service. And we got the following characteristics from fatigue crack growth test carried out in the environment of room and low temperature at $25^{\circ}C$, -3$0^{\circ}C$, -6$0^{\circ}C$, -10$0^{\circ}C$ and -12$0^{\circ}C$ and in the range of stress ratio of 0.05 and 0.3 by means of opening mode displacement. At the constant stress ratio, the threshold stress intensity factor range ${\Delta}K_{th}$ in the early stage of fatigue crack growth (Region I) and stress intensity factor range ${\Delta}K$ in the stable of fatigue crack growth (Region II) was increased in proportion to descent temperature. It assumed that the fatigue resistance characteristics and fracture strength at low temperature is considerable higher than that of room temperature in the early stage and stable of fatigue crack growth region. The straight line slope relation of logarithm da/dN $-{\Delta}K$ in Region II, that is, the fatigue crack growth exponent m increased with descending temperature at the constant stress ratio. It was assumed that the fatigue crack growth rate da/dN in proportion to descending temperature in Region II and the cryogenic-brittleness greatly affect a material with decreasing temperature.

• 동력기계공학회지
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• 제4권1호
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• pp.81-87
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• 2000

In this study, CT specimens were prepared from ASTM SA516 Gr. 70 which was used for pressure vessel plates for room and low temperature service. And we got the following characteristics from fatigue crack growth test carried out in the environment of room and low temperature at $25^{\circ}C,\;-60^{\circ}C,\;-80^{\circ}C\;and\;-100^{\circ}C$ and in the range of stress ratio of 0.05 by means of opening mode displacement. At the constant stress ratio, the threshold stress intensity factor range ${\Delta}K_{th}$ in the early stage of fatigue crack growth (Region I) and stress intensity factor range ${\Delta}K$ in the stable of fatigue crack growth (Region II) was increased in proportion to descend temperature. It assumed that the fatigue resistance characteristics and fracture strength at low temperature is considerable higher than that of room temperature in the early stage and stable of fatigue crack growth region. The straight line slope relation of logarithm $d{\alpha}/dN\;-{\Delta}K$ in Region II, that is, the fatigue crack growth exponent m increased with descending temperature at the constant stress ratio. It assumed that the fatigue crack growth rate $d{\alpha}/dN$ is rapid in proportion to descend temperature in Region II and the cryogenic-brittleness greatly affect a material with decreasing temperature.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2001년도 춘계학술발표대회 개요집
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• pp.224-227
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• 2001

In this study, CT specimens were prepared hem ASTM SA516 which was used for pressure vessel plates for room and low temperature service. And we got the following characteristics from fatigue crack growth test carried out in the environment of room and low temperature at $25^{\circ}C$, -3$0^{\circ}C$, -6$0^{\circ}C$, -8$0^{\circ}C$, -l$0^{\circ}C$ and -l2$0^{\circ}C$ and in the range of stress ratio of 0.1, 0.3 by means of opening mode displacement. At the constant stress ratio, the threshold stress intensity factor range $\Delta K_{th}$ in the early stage of fatigue crack growth ( Region I ) and stress intensity factor range $\Delta$K in the stable of fatigue crack growth ( Region II) was increased in proportion to descend temperature. It assumed that the fatigue resistance characteristics and fracture strength at low temperature is considerable higher than that of room temperature in the early stage and stable of fatigue crack growth region. The straight line slope relation of logarithm da/dN - $\Delta$K in Region II, that is, the fatigue crack growth exponent m increased with descending temperature at the constant stress ratio. It assumed that the fatigue crack growth rate da/dN is rapid in proportion to descend temperature in Region H and the cryogenic-brittleness greatly affect a material with decreasing temperature.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2001년도 춘계학술대회 논문집
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• pp.320-325
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• 2001

In this study, CT specimen were prepared from Pressure Vessel Steel which was used for pressure vessel plates for room and low temperature service. And we got the following characteristics from fatigue crack growth test carried out in the environment of room and low temperature at $25^{\circ}C$, -3$0^{\circ}C$, -6$0^{\circ}C$, -8$0^{\circ}C$, -10$0^{\circ}C$ and -12$0^{\circ}C$ and in the range of stress ratio of 0.05 and 0.3 by means of opening mode displacement. At the constant street ratio, the threshold stress intensity factor range ΔK$_{th}$ in the early stage of fatigue crack growth(Region I) and stress intensity factor range ΔK in the stable of fatigue crack growth(Region II) was increased in proportion to descend temperature. It assumed that the fatigue resistance characteristics and fracture strength at low temperature is considerable higher than that of room temperature in the early stage and stable of fatigue crack growth region. The straight line slope relation of logarithm do/dN -ΔK in RegionII, that is, the fatigue crack growth exponent m increased with descending temperature at the constant stress ratio. It was assumed that the fatigue crack growth rate do/dN is rapid in proportion to descending temperature in Region IIand the cryogenic-brittleness greatly affect a material with decreasing temperature.e.greatly affect a material with decreasing temperature.

• 한국지반공학회논문집
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• 제38권8호
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• pp.7-15
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• 2022

대부분의 선행연구는 동결 삼축압축시험 수행 시, 몰드를 사용하여 시료를 조성하고 단방향으로 동결을 진행하였다. 이는 동결된 시료에 잔류응력이 발생할 가능성이 있기 때문에 인공동결공법이 적용된 지반을 모사하는데 한계가 있다. 본 연구에서는 기존 시험방법의 한계를 보완할 수 있는 시험장비 및 시험방법을 제안하고, 제안된 방법으로 온도 및 구속압력에 따른 동결 사질토의 역학적 특성을 평가하였다. 동결온도가 낮아질수록 동결 사질토는 취성이 증가하였고, 부동수분의 감소 및 얼음자체의 강도 증가로 인하여 강도가 증가하였다. 구속압력의 증가는 강도저감 효과를 발생시키는 압력융해 현상과 강도증진 효과를 발생시키는 흙 입자의 마찰력 증가 모두를 야기하였다. 이처럼 동결 사질토의 역학적 거동은 구속압력과 동결온도의 복합적인 영향을 받는 것으로 나타났다.

• Composites Research
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• 제36권4호
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• pp.246-252
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• 2023

멤브레인 형 LNG 화물창시스템(Cargo containment system, CCS) 내 유리섬유 강화 복합재료 기반 2차 방벽 설치 시 본딩 자동화 머신(automatic bonding machine, ABM) 활용한 prolonged 구조임과 동시에 양단 접착 고정 사이 비 접착(non-bonding, N-B) 영역의 복합재에서 극저온 열 수축 기인한 상당한 열 응력이 발생하기 때문에 이를 고려한 구조 안전성평가 관점에서 수행된 연구가 있으나 실제로 무한히 긴 길이 고려한 기계적 물성 평가를 수행한 연구는 찾아볼 수가 없었다. 해당 복합재는 파단강도 분산이 큰 세라믹 재료 취성 파괴임을 고려하여 2-파라미터 Weibull 통계분석을 통해 실제 길이 대상 신뢰도 있는 기계적 물성치 값을 표준화 하였으며 LNG 운반 환경을 고려한 극저온 환경까지의 특정 온도별 단축 인장실험을 수행하였다. 실험결과, -70℃에서 기계적 강도가 -20℃에 비해 약 1.5배 급증하고 초기 권축 섬유 신장의 비선형 거동이 억제되었다. 또한, 극저온 환경까지 온도가 낮아질수록 기계적 강도는 계속해서 증가하였으나 반대로 연신은 줄어드는 저온 취성의 현상이 확인되었다. 본 연구에서 제시하는 기계적 물성치 데이터는 멤브레인 형 LNG 화물창 구조 안전성 평가 시 신뢰도 높은 해석 지원 물성치 확보 측면에서 유용하게 적용되어지리라 사료된다.