• Geomechanics and Engineering
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• 제24권2호
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• pp.157-166
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• 2021

This paper aims at the temperature and slenderness ratio effects on physical and mechanical properties of Beishan granite. A series of uniaxial compression tests with various slenderness ratios and temperatures were carried out, and the acoustic emission signal was also collected. As the temperature increases, the fracture aperture of intercrystalline cracks gradually increases, and obvious transcrystalline cracks occurs when T > 600℃. The failure patterns change from tensile failure mode to ductile failure mode with the increasing temperature. The elastic modulus decreases with the temperature and increases with slenderness ratio, then tends to be a constant value when T = 1000℃. However, the peak strain has the opposite evolution as the elastic modulus under the effects of temperature and slenderness ratio. The uniaxial compression strength (UCS) changes a little for the low-temperature specimens of T < 400℃, but a significant decrease happens when T = 400℃ and 800℃ due to phase transitions of mineral. The evolution denotes that the critical brittle-ductile transition temperature increases with slenderness ratio, and the critical slenderness ratio corresponding to the characteristic mechanical behavior tends to be smaller with the increasing temperature. Additionally, the AE quantity also increases with temperature in an exponential function.

• 한국표면공학회지
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• 제37권4호
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• pp.226-233
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• 2004

The residual stresses on the surfaces of low carbon 12Cr steels used as a nuclear steam turbine blade material have been studied by controlling the flame hardening surface treatments. The temperature cycles on the surfaces of 12Cr steel were controlled precisely as a function of both the surface temperature and cooling rate. The final residual stress state generated by flame hardening was dominated by two opposite competitive contributions; one is tensile stress due to phase transformation and the other is compressive stress due to thermal contraction on cooling. The optimum processing temperatures required for the desirable residual stress and hardness were in the range of $850^{\circ}C$ to $960^{\circ}C$ on the basis of the specification of GE power engineering. It was also observed that the high residual tensile stress generated by flame hardening induced the cracks on the surfaces, especially across the prior austenite grain boundaries, and the material failure virtually, which might limit practical use of the surface engineered parts by flame hardening.

• 한국안전학회지
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• 제31권3호
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• pp.8-15
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• 2016

The purpose of this study is to design a model with the structural stability so as not to lose the operational function due to structural plastic or fail of a sliding blast door by blast pressure to this aim, a numerical simulation was performed using full-size experiments and M&S (Modeling & Simulation) of the sliding blast door. The sliding blast door ($W3,000{\times}H2,500mm$) under the blast load is in the form of a sliding type 2-way metal grill, which was applied by a design blast pressure (reflected pressure $P_r$) of 17 bar. According to the experimental results of a real sliding blast door under blast load, the blast pressure reached the sliding blast door approximately 4.3 ms after the explosion and lasted about 4.0 ms thereafter. The maximum blast pressure($P_r$) was 347.7 psi (2,397.3 kPa), it is similar to the UFC 3-340-02 of Parameter(91 %). In addition, operation inspection that was conducted for the sliding blast door after real test showed a problem of losing the door opening function, which was because of the fail of the Reversal Bolt that was installed to prevent the shock due to rebound of the blast door from the blast pressure. According to the reproduction of the experiment through M&S by applying the blast pressure measurement value of the full-size experiments, the sliding blast door showed a similar result to the full-size experiment in that the reversal bolt part failed to lose the function. In addition, as the pressure is concentrated on the failed reversal bolt, the Principal Tensile Failure Stress was exceeded in only 1.25 ms after the explosion, and the reversal bolt completely failed after 5.4 ms. Based on the result of the failed reversal bolt through the full-size experiment and M&S, the shape and size of the bolts were changed to re-design the M&S and re-analyze the sliding blast door. According to the M&S re-analysis result when the reversal bolt was designed in a square of 25 mm ($625mm^2$), the maximum pressure that the reversal bolt receives showed 81% of the principal tensile failure stress of the material, in plastic stage before fail.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2005년도 춘계학술대회 논문집
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• pp.275-278
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• 2005

INCONEL 718, nickel based superalloy, has good formability, high strength, excellent corrosion resistance and mechanical properties at high temperature. Owing to theses attractive properties, it finds use in applications such as combustion system, turbine engines and nuclear reactors. In such applications, components are typically required to be tolerant of high stress impact loading. This may cause material degradation and lead to catastrophic failure during service operation. In order to design optimal structural parts made of INCONEL 718, accurate understanding of material's mechanical properties, dynamic behavior and fracture characteristic as a function of strain rates are required. This paper concerned with the dynamic material properties of the INCONEL 718 for the various strain rates. The dynamic response of the INCONEL 718 at intermediate strain rate is obtained from the high speed tensile test machine test and at the high strain rate is from the split Hopkinson pressure bar test. Based on the experimental results, the effects of strain rate on dynamic flow stress, work hardening characteristics, strain rate sensitivity and elongation to the failure are evaluated. Experimental results from both quasi-static and high strain rate up to the 5000/sec are interpolated in order to construct the Johnson-Cook model as the constitutive relation that should be applied to simulate and design the structural parts made of INCONEL 718.

• 한국융합학회논문지
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• 제5권1호
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• pp.1-8
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• 2014

본 논문의 목적은 진동 피로해석 기법을 적용하여 다수의 용접점을 포함하고 있는 점용접 구조물의 강성변화를 고려하여 피로수명을 평가하는 것이다. 먼저 모재부 인장특성 및 점용접부의 인장 및 피로특성을 획득하였다. 유한요소법을 적용하여 S-N 선도를 획득하여 피로해석에 적용하였다. 주파수 응답해석을 수행하여 구조물의 전달함수를 획득하였고, 주파수영역에서 0.11의 PSD를 선정하여 수행하였다. 강성변화 및 고유진동수의 변화를 알아보기 위하여 점용접부의 총 6개 지점 중 최소수명이 발생하는 지점을 기준으로 1개씩 제거하여 반복 해석을 수행하였다. 따라서 강성이 낮아질수록 고유주파수도 낮아지는 것을 확인하였다. 이러한 조건하에서 진동피로해석을 수행하여 피로손상의 누적에 따른 전달합수의 변화를 고려한 진동피로해석을 수행하였다.

• 터널과지하공간
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• 제29권3호
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• pp.172-183
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• 2019

Hoek et al.(2002)이 개발한 일반화된 Hoek-Brown(GHB) 파괴기준식은 암반의 파괴응력 조건을 정의하는 비선형 함수이다. 관련 강도정수들은 GSI 지수값을 이용하여 체계적으로 결정된다. GSI 지수는 현장 암반의 상태를 정량화한 수치이므로 GHB 파괴기준식은 현장의 암반조건을 파괴기준식에 반영할 수 있는 실용적인 암반파괴함수이다. 대부분의 암반공학 기술자들이 선형 Mohr-Coulomb 파괴기준식에 익숙하며, 다수의 암반공학 소프트웨어들이 Mohr-Coulomb 식을 채택하고 있음을 고려하여 등가마찰각과 등가점착력 계산식이 GHB 파괴기준식 발표와 함께 제시되었다. 그러나 이 목적으로 제시된 등 가마찰각 및 등가점착력 계산식은 선형 최적화가 수행되는 최소주응력 범위의 하한 값을 암반의 인장강도로 고정시키고 있다. 따라서 해석영역에 인장응력이 분포하지 않은 경우 Hoek et al.(2002)의 제안식을 이용한 등가마찰각 및 등가점착력 산정결과는 정확성이 떨어질 수 있다. 이러한 기존 등가마찰각 및 등가점착력 산정수식의 단점을 극복하기 위하여 이 연구에서는 임의의 최소주응력 구간에 대해서도 최적 등가마찰각과 등가점착력을 계산할 수 있는 해석적 수식을 유도하고 결과식의 정확성을 검증하였다.

• 한국정밀공학회지
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• 제13권8호
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• pp.96-101
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• 1996

Glass fiber reinforced polymeric composites hold considerable promise for increased use in low cost high volume applications because of the potential for processing by solid phase forming. Unfortunately, because of the wide variety of such materials, inherent bariability in properties, and complex temperature and strain rate dependence, large strain behavior of these materials has not been well characterized. Of particular importance is failure during processing due to localized necking instability, and it is this phenomenon that is primary focus of this study. The strain rate and temperature dependence is used to predict limiting tensile strains, based on Mackinack imperfection theory. Excellent correlation was obtained between theory and experiment, and the results are summarized in the limit strains as a function of temperature and stain rate.

• 콘크리트학회논문집
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• 제17권6호
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• pp.911-922
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• 2005

섬유보강 콘크리트 보의 전단강도와 거동 특성을 규명하기 위해서 이론적 연구를 수행하였다. 섬유보강 콘크리트 보의 단면에 작용하는 전단력은 압축대와 인장대에 의해서 지지된다. 압축대의 전단성능은 단면의 휨모멘트에 의해서 발생하는 수직응력과의 상관관계를 고려하여 정의하였으며, 인장대의 전단성능은 섬유보강 콘크리트의 균열 후 인장강도를 고려하여 정의하였다. 보의 휨변형에 따라서 수직응력의 크기와 분포가 변화하므로, 보의 전단성능은 휭변형의 함수로 정의하였다. 전단성능곡선과 전단요구곡선의 교점에서, 보의 전단강도와 위험단면의 위치가 결정된다. 제안된 설계 방법은 섬유보강 콘크리트와 일반 콘크리트 보를 위한 통합전단강도모델로 사용 할 수 있다.

• 한국건설순환자원학회논문집
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• 제7권4호
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• pp.316-322
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• 2019

본 연구에서는 환경적·물리적 인자들의 불확실성을 반영하는 확률론적 접근법을 적용하여, 원자로 가동기간 동안 장시간 방사능에 노출된 원전 콘크리트 차폐벽의 재료적 특징 및 강도에 대한 영향을 평가하였다. 방사화에 따른 콘크리트의 재료적 특성 변화를 조사하였으며, 중성자 노출량과 시간과의 관계를 나타내는 중성자속 분석을 통해 차폐 콘크리트 의 시간의존적 압축강도와 인장강도의 변화를 예측하였다. 압축강도와 인장강도 각각의 변화에 따른 차폐 콘크리트의 파괴확률을 몬테카를로 시뮬레이션(Monte Carlo Simulation) 기법을 적용하여 추정하였다. 본 연구에서는 가동 40년 만인 2017년에 영구정지한 고리 1호기의 해체 안전성 평가를 위해, 이와 유사한 원전유형 및 관련 자료를 활용하여 콘크리트 생체차폐벽의 성능변화를 예측하였다.

• 한국해양공학회지
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• 제19권5호
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• pp.43-49
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• 2005

This paper is to investigate the effect of corrosion by acoustic emission method in tensile loading and the adhesiveness between substrate and coating layer. The powders used are Zn and Amdry625, respectively. They are coated on brass alloy substrate. AE signals of Zn and Amdry625 coating layer increase drastically in strain $2\%$. However, those of Zn specimen have more than those of Amdry625 specimen. When the specimens executed the corrosion test under $3.5\%$ NaCl solution for 500, 1000 hours, the salt solution penetrated into the surface of the substrate through the pores of the coating layer. As a result, corrosion production formed on the surface of the substrate. The adhesiveness between coating layers is weakened by the polarization and corrosion itself. The AE event, count, and energy of corroded coating specimens decrease, compared to specimens without corrosion. The results are summarized as follows : 1. In the tensile tests, the time that it took to start and develop the cracks and exfoliations between the surface of the substrates and the plasma spray coatings were different according to the type of plasma sprayed material, which are Zn and Amdry625. These phenomena were obvious at the strain rate 1 to $5\%$, and few available data were found after that stage. 2. The specimens with Zn coating showed the characteristics of crack, according to the changes of the tensile strength applied on the substrates while those with Amdry625 showed exfoliation as a result of low adaptation to the tensile strength. 3. The anti-corrosion specimens showed that the adhesive properties between the substrate and the plasma spray coating were strong in the order of Zn, Amdry. It showed that Corroded specimens cracked or exfoliated easily, even with the small energy, because those had a comparatively weakened adhesive property, due to corrosion. 4. Zn specimen showed no corrosion phenomena on the surface of the substrates, because they had the function of sacrifice anode however, Amdry625 specimen showed the corrosion, because it did not have that function.