• 한국안전학회지
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• 제9권4호
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• pp.11-16
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• 1994

Acoustic emission technique is applied to the fatigue crack initiation in a carburized gear tooth. Acoustic emission test performed on carburized gear and three-point bending test equal to carburized gear hardness. The marked acoustic emission are detected at the early stage of crack initiation measured by a crack gauge and the final stage just before the tooth failure. The estimated acoustic emission energy rate are characteristic of the measured acoustic emission.

• 열처리공학회지
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• 제9권1호
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• pp.69-77
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• 1996

The fatigue crack initiation behavior of plasma ion nitrided SACM645 steel was investigated through the rotary bending fatigue test and residual stress measurement by XRD. It was shown by XRD and EPMA that the plasma ion nitrided surface was composed of ${\gamma}^{\prime}(Fe_4N)$phase and ${\varepsilon}(Fe_{2-3}N)$phase, and that the nitrogen atoms existed in Fe matrix in diffusion layer. The OM, SEM and Auger spectroscopy showed that the depth of compound layer, mixed compound and diffusion layer, and diffusion layer was $8{\mu}m$, $30{\mu}m$ and $300{\mu}m$, respectively. However, the microhardness test showed that the depth of hardened layer was $500{\mu}m$. The tensile strength of the ion nitrided SACM645 was lower than that of the unnitrided SACM645, and the ion nitrided specimen was fractured without plastic deformation. The nitrided SACM645 showed much poorer low cycle fatigue properties than the unnitrided one. In rotary bending fatigue, the fatigue strength of the ion nitrided SACM645 was higher than that of the unnitrided specimen, and the fatigue crack initiation sites changed by applied fatigue stress levels. The XRD result showed that the ion nitrided SACM645 has the compressive residual stress from surface to $600{\mu}m$ deep and the tensile residual stress from $600{\mu}m$ to deeper site. It is thought that crack initiation takes place at the point where the total stress of residual stress and applied stress is maximum.

• 대한기계학회논문집A
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• 제37권3호
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• pp.429-436
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• 2013

본 논문에서는 고주파 열처리된 SAE1055 베어링강의 경도에 따른 피로 거동 및 이의 확률론적 평가를 수행하였다. 이를 위하여 경도 수준에 따른 5 종류의 시험편(A : 원재료, B : HV390-전경화, C : HV510-전경화, D : HV700-전경화 및 E : HV-700 표면경화)를 준비하였다. 피로시험은 4 점 회전굽힘 피로시험기를 이용하여 응력비 R=-1 의 조건하에서 수행하였다. 그 결과, SAE1055 강의 피로 거동은 경도에 따라 크게 변화하였으나 HV510 수준이상에서는 피로한도의 증가는 관찰되지 않았다. 또한 피로 파손기구에 대한 경도의 영향을 평가하기 위하여 SEM(scanning electron microscope)을 이용한 파면 관찰을 수행하였다. 피로수명의 통계적 특성은 P-S-N(probabilistic S-N) 곡선을 이용하여 평가되었으며 이에 대한 경도의 영향은 잔류치 해석(residue analysis)을 통하여 수행하였다.

• 대한기계학회논문집A
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• 제41권7호
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• pp.635-643
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• 2017

STS 304L 강재의 냉간압연율의 증가에 따라 t가 1.5 mm에서 1.1 mm까지 감소하면 인장강도, 항복강도, 경도치 및 UFT피로시험의 피로한도는 선형적으로 증가하였다. t=1.5 mm, t=1.4 mm, t=1.3 mm 및 t=1.1 mm인 4가지 시험편의 UFT피로시험(R= -1)결과, 회전굽힘피로시험(R= -1)의 결과처럼 $10^6$ 영역에서 S-N곡선의 피로한도가 절점(knee point)을 형성하였고, 기가사이클 피로에서 생기는 현상인 피로한도가 추가로 감소하지않았다. 또 t=1.1 mm인 경우 가장 높은 피로한도 345 MPa로 되었고, 원소재(t=1.5 mm)에 대하여 64.3 % 증가하였다. 냉간압연율에 따른 UFT피로시험결과 많은 작은 표면균열이 티어링(tearing)하면서 발생, 성장, 서로 합체하였다.

• 한국강구조학회 논문집
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• 제12권5호통권48호
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• pp.617-628
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• 2000

이 연구에서는 하중비전달형 필렛용접부를 대상으로 순수휨상태에서 TIG 처리에 따른 피로강도 향상정도 및 피로특성을 정량적으로 평가하기 위해서 4점 휨실험을 실시하였다. 피로실험결과 용접후처리를 실시하지 않은 시험체는 국내 외에서 규정하는 피로강도등급을 만족하고 있고 TIG 처리한 시험체는 용접후처리를 실시하지 않은 시험체보다 $2{\times}106$회 피로강도가 상회하는 것을 알 수 있었다. 또한 비치마크실험결과 피로균열은 용접지단부의 비드접선각도 및 곡률반경이 최소로 되는 점에서 다발적으로 발생하며, 반타원형 균열로 성장, 합체되어 파단에 이르는 것을 확인할 수 있었다. 한편 유한요소해석결과 용접지단부의 응력집중계수는 용접지단부의 비드접선각도 및 곡률반경과 밀접한 관계가 있으며, 이 중에서 곡률반경이 용접지단부의 응력집중계수에 보다 큰 영향을 미치는 것을 알 수 있었다. 한편 파괴역학적 해석결과 a/t가 0.4 이하인 경우에 기하학적형상보정계수가 균열보정계수에 가장 지배적인 영향을 미치는 인자임을 알 수 있었다. 또한 유한요소해석결과로부터 산정한 응력확대계수범위와 피로균열성장속도의 관계식으로부터 피로수명을 비교적 정확하게 산정할 수 있었다.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2006년도 춘계학술발표회 논문집(I)
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• pp.282-285
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• 2006

This study is to examine bond strength of beam reinforced with GFRP rebar under 4-point bending test by adopting BRITISH STANDARD. The variables were made to have bonding length of 5times$(5d_b)$, 10times$(10d_b)$ and 15times$(15d_b)$ of the nominal diameter of GFRP rebar and were done to analyze the relationship between the bonding strength and the slip. In the result of the test, pull-out failure was dominant in the $5d_b$ and $10d_b$ specimen, both patterns of the pull-out failure and concrete splitting failure appeared in the $10d_b$. On the other hand, the $15d_b$ specimen showed only concrete splitting failure at the end of bonding length. Therefore, it was prove that available bonding length of the GFRP rebar under bending condition on static test is over $15d_b$ then farther research such as fatigue bending test, development of bonding model, FEM parameter study should be performed.

• 한국자동차공학회논문집
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• 제22권2호
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• pp.141-147
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• 2014

This study aims to investigate the influence of bevel angles on the fatigue life of V-groove butt-welded joints with back-plates made by SM490A steel material, generally used for excavators, because changes in the geometry, material and surface properties of welded regions affect the fatigue life of welded structures. Butt type test specimens were prepared by the $CO_2$ welding of rolled steel plates (SM50A steel) with a thickness of 13.5 mm at a welding speed of 30 cm/min and these Butt type test specimens had two different groove angles, which are $40^{\circ}$ (A type) and $30^{\circ}$ (B type). In order to investigate differences in fatigue life between two types, 4-point bending fatigue tests were conducted with a stress ratio of R=0.1 under the cyclic loading environment at a frequency of 5 Hz at room temperature. The fatigue life of A type specimens was approximately 7% higher than that of B type specimens. The stress concentration factors calculated by finite element analysis were 2.16 for A type and 2.25 for B type, whose difference was caused by the influence of the back-plates of butt-welded structures. The current results could provide important guidelines to determine the V-groove angle of butt-welded joints with a satisfactory fatigue life, although under severe operating conditions.

• 한국해양공학회지
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• 제6권1호
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• pp.96-104
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• 1992

Aircraft structures and engineering structures are always subject to variable amplitude loads. Variable amplitude loads include some kind of loading history; for example, constant amplitude load, single peak overload and block overload etc. Crack growth under variable amplitude loading exhibits retardation effect. In this study, the 4 point bending fatigue test was performed by hydrolic servo fatigue testing machine on 7075-T6 Al-alloy. The retardation effect of overload ratio and numbers of overload cycle was quantitatively studied. 1) Change of retardation effect against increment of overload ratio is more evident when the multiple overload is applied than single overload is done. 2) The number of overload cycle is very important factor about the crack growth retardation effect when the overload ratio is more than 1.75; that is not when the overload ratio is less than 1.75. 3) Overload affected zone size increased gradually by increment of crack growth retardation effect. 4) Crack driving force is more greatly reduced when the crack tip branched off two direction than it sloped to one direction.

• 한국정밀공학회지
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• 제29권3호
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• pp.307-312
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• 2012

This study aims to investigate the effect of the post weld treatments on the fatigue life of T-type welded structure made by a SM50A steel material, generally used for excavators, because changes in the geometry, material and surface properties of welded regions affect the fatigue life of welded structures. T-type test specimens were prepared by the CO2 welding of rolled steel plates (SM50A steel) with a thickness of 10 mm at a welding speed of 30 cm/min and these Ttype welded specimens were further treated by UIT (Ultrasonic Impact Treatment) and/or toegrinding post welding treatment methods. In order to investigate improvements on the fatigue life of the samples. 3-point bending fatigue tests were conducted with a stress ratio of R=0.1 under a cyclic loading environment at a frequency of 5 Hz, via a hydraulic fatigue testing machine (${\pm}100\;kN$, MTS 809). The tests were performed at room temperature. The fatigue life of UIT specimens was approximately 25 times longer than that of as-welded specimens at a stress amplitude of 281 MPa, while toe-grinding specimens exhibited 4.15 times longer fatigue life. The current results could provide important guidelines to determine the proper post weld treatment methodologies of T-type welded parts for excavators with a satisfactory fatigue life although under severe operating conditions.

• 한국구조물진단유지관리공학회 논문집
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• 제12권1호
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• pp.101-108
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• 2008

본 연구에서는 철근과 같은 기계적 맞물림 현상을 활용하기 위하여 이형리브가 형성되어 있는 GFRP 보강근을 제작하여 철근대체 재료로 사용하기 위해 FRP 보강근의 부착성능을 규명하고자 한다. 하지만 지금까지 많은 기존 연구자들이 부착성능에 대한 실험으로 단순 1방향(수직, 수평)인장실험으로 철근과 콘크리트 또는 FRP 보강근과 콘크리트사이의 부착특성을 고찰하여 두 재료 사이의 부착-슬립에 관한 제안식을 도출해왔다. 국내에서는 아직까지 GFRP 보강근의 부착에 대한 관심이 증대대고 있는 실정이지만 피로부착에 관한연구는 미흡한 편이이어서 GFRP 보강근의 피로 연구가 필요로 하다. 본 연구에서는 BRITISH STANDARD에서 규정하고 있는 방법에 의하여 휨 부착 시험체를 제작하여 정적 휨 부착실험 최대파괴하중의 70% ~ 90%의 하중으로 반복하중재하 후 정적실험을 통하여 GFRP로 보강된 콘크리트 피로부착 성능을 검증하였다.