• Journal of Welding and Joining
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• v.20 no.6
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• pp.106-106
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• 2002

This study investigated variations of micro-structures and mechanical properties of Ti / STS321L joint with various bonding temperature and time using brazing method. According to increasing bonding temperature and time, it was observed that the thickness of their reaction layer increased due So increasing diffusion rate and time. From the EPMA results, Ti diffused to the STS321L substrate according to increasing bending time to 30min. Hardness of bonded interface increased with increasing bonding temperature and time due to increasing their oxides and intermetallic compounds. XRD data indicated that Ag, Ag-Ti intermetallic compounds, TiAg and Ti₃Ag and titanium oxide, TiO₂were formed in interface. In tensile test, it was found that the tensile strength had a maximum value at the bonding temperature of 900℃ and time of 5min, and tensile strength decreased over bonding time of 5min. The critical thickness of intermetallic compounds was observed to about 30㎛, because of brittleness from their excessive intermetallic compounds and titanium oxide, and weakness from void.

• Proceedings of the KWS Conference
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• 1996.10a
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• pp.3-15
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• 1996

The formation of a thicker hard alloyed layer have been investigated on the surface of aluminum cast alloy (AC2B) by PTA overlaying process with Cr, Cu and Ni motel powders under the condition of overlaying current 125-200A. overlaying speed 150 mm/min and different powder feeding rate 5-20 g/min. In addition the characteristics of hardening and wear resistance of alloyed layer here been examined in relation to the microstructure of alloyed layer. Main results obtained were summarized as follows: 1) There was an optimum overlaying condition to get a good alloyed layer with smooth surface. This good layer became easy to be formed as increasing overlaying current and decreasing powder feeding rate under a constant overlaying speed. 2) Cu powder was the most superior one in metal powders used due to a wide optimum overlaying condition range, uniform hardness distribution of Hv250-350, good oar resistance and freedom from cracking in alloyed layer with fine hyper-eutectic structure. 3) On the contrary, irregular hardness distribution was usually obtained in Cr ar Ni alloyed layers of which hardness was increased as Cr or Ni contents and reached to maximum hardness of about Hv400-850 at about 60wt%cr or 40wt%Ni in alloyed layer. 4) Cracking occurred in Cr or Ni alloyed layers with higher hardness than Hv250-300 at mere than 20-25wt% of Cr or Ni contents in alloyed layer. Porosity was observed in all alloyed layers but decreased by usage of spherical powder with smooth surface.

• Journal of Korean Society of Steel Construction
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• v.25 no.5
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• pp.569-578
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• 2013

In a super-tall building construction, thick and large-sized embed plates are usually used to connect mega structural steel members to RC core wall or columns by welding a gusset plate on the face of the embed plate with T-shape. A large amount of heat input accumulated by weld passes causes the plates to expand or deform. In addition, the temperature of concrete around the plates also could be increased. Consequently, cracks and spalls occur on the concrete surface. In this study, the effect of weld heat on embed plates and 80MPa high strength concrete is investigated by considering weld position (2G and 3G position), edge distance, concrete curing time, etc. Measured temperature of the embed plates was compared with the transient thermal analysis results. Finally, push-out tests were performed to verify and compare the shear studs capacity of the embed plate with design requirement. Test result shows that the shear capacity of the plate is reduced by 14%-19% due to the weld heat effect and increased as the concrete curing time is longer.

• Proceedings of the KWS Conference
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• 2009.11a
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• pp.39-39
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• 2009

고강도강의 용접성은 저온균열 저항성으로 대변되는데, TMCP강과 HSLA강 등이 개발되면서 고강도강의 저온균열저항성이 크게 향상되어 무예열 용접성이 확보되었다. 그러나 용접재료 측면에서는 그에 상응하는 재료의 개발이 지연되어 용착금속부에서의 저온균열이 심각한 문제로 대두되고 있는 실정이다. 이러한 문제는 800 MPa급인 HY-100강재를 HSLA-100강으로 대체하는 과정에서 현실적인 문제로 제기 되었다. 즉 HSLA강은 용접 예열이 필요치 않았으나 기존의 용접재료, 즉 HY-100 강재에 사용하던 용접재료를 사용하게 되면 용착금속부에서 저온균열이 발생하여 용접예열을 생략할 수 없다는 판단에 이르게 되었던 것이다. 이에 본 연구의 목적은 HSLA-100강을 무예열 용접할 수 있는 GMA 용접와이어 개발하는 것이며, 구체적인 개발 목표는 무예열 용접조건에서 800 MPa 이상의 인장강도를 가지며 $-50^{\circ}C$에서의 충격인성이 50 J 이상인 GMA 용접와이어 개발하는 것이다. 이러한 용접재료를 합금설계함에 있어 무예열 용접성을 확보하기 위하여 용접재료의 탄소함량을 0.01% 수준으로 하고, 용착금속의 인장강도와 저온 충격치에 미치는 Mn과 Mo 함량의 영향을 검토하고 각각의 조성을 실험계획법으로 확정하였다. 그리고 확산성수소량에 따른 저온균열 발생 여부를 확인하여 무예열용접성을 확보하기 위해서는 확산성수소량이 3ml/100g 이하가 되어야 한다는 사실을 실험적으로 확인하였다. 그리고 이를 달성하기 위해서는 원자재인 와이어로드의 표면 품질이 중요하다는 사실도 확인할 수 있었다. 다음으로는 실험계획법에 의거하여 선정된 합금조성의 신뢰성을 검증하기 위하여 800kg 중량의 시제품을 생산하였으며, 생산된 시제품에 대해서는 실험계획법에서 사용한 Ar+5%CO2외에도 Ar+20%CO2를 적용하여 보호가스의 영향을 검토하였다. 검토 과정에서 Ar+20%CO2용으로 사용하기 위해서는 용접재료의 Si 및 Mn 함량이 상향조정되어야 함을 확인할 수 있었다. 그리고 탄소함량을 0.05% 수준으로 증가시키면 Mo 함량을 크게 저하시킬 수 있음도 확인할 수 있었다. 이러한 과정을 거쳐 개발된 GMA 용접재료는 무예열 용접조건에서 저온균열이 발생하지 않았으며, 인장강도는 830 MPa이었으며 $-50^{\circ}C$에서의 충격치는 90 J 이상이었다.

• Journal of Welding and Joining
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• v.31 no.1
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• pp.58-64
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• 2013

The following results were obtained, microstructures and tensile properties in arc brazed joints of DP(dual phase) steel using Cu-5.3wt%Sn insert metal was investigated as function of brazing current. 1) The Fusion Zone was composed of ${\alpha}Fe+{\gamma}Cu$ and Cu23Sn2. The reason for the formation of these solid solutions. Despite, Fe & Cu were impossible to solid solution at room temperature. It's melting & reaction to something of insert metal & Base Metal (DP Steel) by Arc. Brazing Process has faster cooling rate then Cast Process, Supersaturated solid solution at room temperature. 2) The increase Hardness of Fusion Zone was directly proportional to the rise of welding current. Because, ${\alpha}Fe+{\gamma}Cu$ phase (higher hardness than the Cu23Sn2.(104.1Hv < 271.9Hv)) Volume fraction was Growth, due to increasing the amount of base metal melting by High current. 3) The results of tensile shear test by Brazing, All specimens happen to fracture in Fusion Zone. On the other hand, when Brazing Current increasing tend to rise tensile load. but it was very small, about 26-30% of the base metal. 4) The result of fracture analysis, The crack initiate at Triple Point for meet to Upper B.M/Under B.M/Fusion Zone. This Crack propagated to Fusion zone. So ruptured by tensile strength. The Reason to in the fusion zone fracture, Fusion zone by Brazing of hardness (strength) was very lower then the base metal (DP steel). In addition the Fusion Zone's thickness in triple point was thin than the base metal's thickness in triple point.

• Journal of Welding and Joining
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• v.12 no.4
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• pp.85-101
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• 1994

Effect of Cr, Cu and Ni metal powders addition on the alloyed layer of aluminum alloy (AC2B) has been investigated with the plasma transferred arc (PTA) overlaying process. The overlaying conditions were 125-200A in plasma arc current, 150mm/min in process speed and 5-20g/min in powder feeding rate. Main results obtained are summarized as follows: 1) It was made clear that formation of thick surface alloyed layer on aluminum alloy is possible by PTA overlaying process. 2) The range of optimum alloying conditions were much wider in case of Cu and Ni powder additions than the case of Cr powder addition judging from the surface appearance and the bead macrostructure. 3) Alloyed layer with Cu showed almost the homogeneous microstructure through the whole layer by eutectic reaction. alloyed layers with Cr and Ni showed needle-like and agglomerated microstructures, the structure of which has compound layer in upper zone of bead by peritectic and eutectic-peritectic reactions, respectively. 4) Microconstituents of the alloyed layer were analyzed as A1+CrA $l_{7}$ eutectics, C $r_{2}$al sub 11/, CrA $l_{4}$, C $r_{4}$A $l_{9}$ and C $r_{5}$A $l_{*}$ 8/ for Cr addition, Al+CuA $l_{2}$(.theta.) eutectics and .theta. for Cu addition, and Al+NiA $l_{3}$ eutectics. NiA $l_{3}$, N $i_{2}$A $l_{3}$ and NiAl for Ni addition. 5) Concerning defect of the alloyed layer, many blow holes were seen in Cr and Ni additions although there was lesser in Cu addition. Residual gas contents in blow hole for Cu and Ni alloyed layer were confirmed as mainly $H_{2}$ and a littie of $N_{2}$ Cracking was observed in compound zone of the alloyed layer in case of Cr and Ni addition but not in Cu alloyed layer.r.r.

• Journal of Welding and Joining
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• v.12 no.4
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• pp.102-109
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• 1994

The thick and hard alloyed layer was formed on the surface of Aluminum Cast Alloy(AC2B) by PTA overlaying process with Cr, Cu and Ni metal powders under the condition of overlaying current 150A, overlaying speed 150mm/min and different powder feeding rate 5-20g/min. The characteristics of hardening and were resistance of alloyed layer have been investigated in relation to microstructure of alloyed layer. As a result, it was made clear that Cu powder was the most superier one in three metal powders used due to an uniform hardness distribution of Hv 250-350, good wear resistance and freedom from cracking in alloyed layer of which microstructure consisted of hypereutectic. On the contrary, irregular hardness distribution was usually obtained in Cr or Ni alloyed layers of which hardness was increased as Cr or Ni contents and reached to maximum hardness of about Hv 400-850 at about 60wt% Cr or 40wt% Ni in alloyed layer. However the cracking occurred in these alloyed layers with higher hardness than Hv 250-300 at more than 20-25wt% of Cr or Ni contents in alloyed layer. Wear rate of alloyed layer was decreased to 1/10 in Cu alloyed layer and 1/5 or 1/3 in Cr or Ni alloyed layer with same hardness of about Hv 300 in comparison with that of base metal at higher sliding speed.

• International Journal of Automotive Technology
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• v.5 no.1
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• pp.55-59
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• 2004

Spot welding is a very important and useful technology in fabrication of thin sheet structures such as the parts in an automobile. However, because the fatigue strength of the spot welding point is considerably lower than that of the base metal due to stress concentration at the nugget edge, the nugget size must be estimated to evaluate a reasonable fatigue strength at a spot welded lap joint. So far, many investigators have experimentally studied the estimation of fatigue strengths of various spot weldments by using a destructive method. However, these destructive methods poses problems so testing of weldments by these methods are difficult. Furthermore, these methods cannot be applied to a real product, and are time and cost consuming, as well. Therefore, there has been a strong, continual demand for the development of a nondestructive method for estimating nugget size. In this study, the effective nugget size in spot weldments have been analyzed by using thermoelastic stress analysis adopting infrared thermography. Using the results of the temperature distribution obtained by analysis of the infared stress due to adiabatic heat expansion under sinusoidal wave stresses, the effective nugget size in spot welded specimens were estimated. To examine the evaluated effective nugget size in spot weldments, it was compared with the results of microstructure observation from a 5％ Nital etching test.

• Proceedings of the KWS Conference
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• 2009.11a
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• pp.95-95
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• 2009

Zinc coatings provide the most effective and economical way of protecting steel against corrosion. There are three types of galvanizing lines typically used in production line in galvanizing industries,Galvanize (GI) coating (Zn-0.1-0.3%Al), Galfan coating (Zn-5%Al), Galvalume(GL) coating (45%Zn-Al). In continuous Galvanizing lines, the immersed bath hardware (e.g. bearings, sink, stabilizer, and corrector rolls, and also support roll arms and snout tip) are subjected to corrosion and wear failure. Understanding the reaction of these materials with the molten Zn alloy is becomes scientific and commercial interest. To investigate the reaction with molten Zn alloys, static immersion test performed for 4, 8, 16, and 24 Hr. Two different baths used for the static immersion, which are molten Zn and molten Zn-55%Al. Microstructures characterization of each of the materials and intermetallic layer formed in the reaction zone was performed using optical microscope, SEM and EDS. The thickness of the reaction layer is examined using image analysis to determine the kinetics of the reaction. The phase dominated by two distinct phase which are eutectic carbide and matrix. The morphology of the intermetallic phase formed by molten Zn is discrete phase showing high dissolution of the material, and the intermetallic phase formed by Zn-55wt%Al is continuous. Aluminum reacts readily with the materials compare to Zinc, forming iron aluminide intermetallic layer ($Fe_2Al_5$) at the interface and leaving zinc behind.

• Proceedings of the KWS Conference
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• 2009.11a
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• pp.46-46
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• 2009

과거 고강도강 용접부에서 발생하는 저온균열은 주로 용접열영향부에서 발생하였는데, 이러한 문제점을 해결하기 위하여 강재 메이커들은 고강도강의 용접성을 향상시키고자 노력하였다. 이러한 노력의 결과로 TMCP, HSLA 강 등이 개발되었고 이들 강재는 예열온도를 저하시킬 수 있다는 장점 때문에 보편화되어 사용되었다. 이러한 강재는 모재 예열온도를 기준으로 적용하게 되면 용착금속에서 저온균열이 발생하는 경우가 있다. 따라서 이제는 용접재료의 용접성, 즉 용접재료의 저온균열 저항성을 평가 할 수 있는 기법이 요구된다. 본 연구의 목적은 용착금속의 저온균열 저항성을 평가하는 것인데, 저온균열 저항성은 용착금속의 미세조직에 따라 다르게 나타날 수 있다. 용착금속의 합금조성은 기본적으로 용착금속에 요구되는 최저 강도와 충격인성을 만족할 수 있도록 설계한다. 하지만 유사한 강도의 유사한 합금조성이더라도 일부 합금 성분에 의해 용착금속의 미세조직들은 상이하게 나타날 수 있는데, 미세조직 특성에 의하여 용착금속의 강도와 저온인성이 결정된다. 용착금속의 저온균열 저항성을 평가하기위하여 Gapped Bead-on-Groove(G-BOG) 시험에 사용된 모재는 50mm 두께의 mild steel을 사용하였으며, 모재의 희석을 방지하기위해 15mm 깊이로 V-groove 가공 후 buttering 용접 하였다. 용접된 시편은 다시 5mm 깊이로 V-groove로 2차 가공 후 Ar + 20% $Co_2$ gas를 사용하여 용접하였다. 용접재료는 ER-100S-G grade로 비슷한 합금조성을 갖는 2 종류를 사용하였다. A용접재료는 Ti 이 0.1% 함유 되었으며, B용접재료는 Ti 함유되지 않은 것을 사용하였다. 또한 예열 온도에 따라 저온균열 감수성을 평가하기위하여 모재의 예열온도를 각각 상온, $50^{\circ}C,\;75^{\circ}C,\;100^{\circ}C$로 하여 실험을 진행하였다. 용착금속의 미세조직을 확인해본 결과 Ti 함유된 A 용착금속 미세조직은 대부분 침상형페라이트로 나타났으며, Ti 함유되지 않은 B 용착금속 미세조직은 대부분 베이나이트로 나타났다. G-BOG 시험 결과 Ti 함유된 A 시편이 Ti 함유되지 않은 B 시편보다 저온균열 발생량이 적었다. 이는 용착금속의 미세조직분포 및 특성에 따라 저온균열감수성이 다르다는 것을 나타낸다.