• Journal of Power System Engineering
• /
• v.11 no.1
• /
• pp.107-114
• /
• 2007

Underwater wet arc welds were experimentally performed on 11mm thick SS400 mild steel plate as base metal by using six different types of flux coated electrodes of 4.0mm diameter; KSKR, KSKT, USBL, JPUW, UWEA, and UWEB. As results, the developed flux coated underwater electrode had a good weldability compared with other domestic terrestrial electrodes. By rapid cooling rate, the hardness value of HAZ were increased by quenching effects. Mechanical properties for the multi-pass butt-welding specimen are also tested experimentally. The feasibility of the developed underwater electrode was experimentally studied and the results achieved in this wet arc welds have shown that the developed wet welding electrode UWEB can have a degree of integrity.

• Journal of Ocean Engineering and Technology
• /
• v.1 no.2
• /
• pp.67-73
• /
• 1987

The feasibility for a practical use of underwater wet arc welding process is experimentally investigated by using low hydrogen and high oxide type electrodes and TMCP steel plates. Main results are summarized as follows: 1)The absorption speed of the coated low hydrogen and high titanium oxide type eletrodes becomes constant after about 30 minutes in water, and more steeping time in water does not influnce welding arc behavior. 2) By bead appearance and X-ray inspection, the high titanium oxide type electrode is better than the low hydrogen type in underwater arc welding process. 3) The mechanical properties of underwater wet arc welds depend upon welding conditions more than those of in-air welds, and the optimum welding condition can be obtained. 4) Because of quenching effect by rapid cooling rate in underwater wet welding, the maximum hardness of HAZ is increased relatively higher in underwater wet welding, process.

• Journal of Welding and Joining
• /
• v.28 no.3
• /
• pp.104-113
• /
• 2010

In this study, to predict the microstructure in weld HAZ of low alloyed steel, prediction model for the phase transformation considering the influence of prior austenite grain size and cooling rate was developed. For this study, six low alloyed steels were designed and the effect of alloying elements was also investigated. In order to develop the prediction model for ferrite transformation, isothermal ferrite transformation behaviors were analyzed by dilatometer system and 'Avrami equation' which was modified to consider the effect of prior austenite grain size. After that, model for ferrite phase transformation during continuous cooling was proposed based on the isothermal ferrite transformation model through applying the 'Additivity rule'. Also, start temperatures of ferrite transformation were predicted by $A_{r3}$ considering the cooling rate. CCT diagram was calculated through this model, these results were in good agreement with the experimental results. After ferrite transformation, bainite transformation was predicted using Esaka model which corresponded most closely to the experimental results among various models. The start temperatures of bainite transformation were determined using K. J. Lee model. Phase fraction of martensite was obtained according to phase fractions of ferrite and bainite.

• Journal of Advanced Marine Engineering and Technology
• /
• v.35 no.1
• /
• pp.75-81
• /
• 2011

Dissimilar joining of aluminum 6061-T6 alloy to aluminum 5083-O alloy was performed using friction-stir welding technique. The mechanical properties, hardness, macro- and micro-structure on dissimilar friction-stir-weld aluminium alloy were investigated. Mechanical properties of the weld mainly depend on which Al alloy is placed at the retreating sides of the rotating tool respectively during dissimilar friction-stir weld because the microstructure of stir zone was mainly composed of welded Al alloys of the retreating side. Onion ring pattern was observed like lamella structure stacked by each Al alloy in turn. It apparently results in defect-free weld zone that traverse speed was changed to 124 mm/min under conditions of tool rotation speed like 1250 rpm with 5 mm of tool's prove diameter, 4.5 mm of prove length, 20 mm of shoulder diameter, and $2^{\circ}$ of tilting angle. The 231 MPa of ultimate stress and the 121 MPa of yield point are obtained about the friction-stir-welded Al 6061-T6(AS) to Al 5083-O(RS).

• Proceedings of the KWS Conference
• /
• 2009.11a
• /
• pp.27-27
• /
• 2009

드라이브 샤프트는 일반적으로 엔진에서 발생된 회전력을 바퀴에 직접 전달하는 동시에 조향기능을 수행하는 자동차 부품이다. 최근에 경량화를 통한 에너지 절감을 위하여 기존 스틸소재를 알루미늄으로 대체하는 방안에 대한 연구가 집중되고 있다. 그러나 알루미늄 단일소재로 드라이브 샤프트를 제조하는 것은 비경제적이며 또한 기 개발된 자동차 부품들과의 연결을 고려하여 알루미늄 튜브와 스틸 요크의 이종금속 접합기술이 요구된다. 전자기 펄스용접은 전자기력을 이용하여 용접대상물을 고속으로 충돌시켜 용접하는 기술로서 열 발생이 적어 재료의 특성차로 인한 결함 및 변형이 발생하지 않아, 이종금속간 고품질 용접이 가능하며, 전자기 펄스 용접부의 품질과 밀접한 관계를 갖는 공정변수 경우 모재와 접합재의 재질 따라 적정 공정변수 범위가 변화되므로 공정에 따른 데이터의 축적은 대단히 중요하다. 전자기 펄스 용접을 이용한 이종금속 접합시 접합부 품질에 영향을 미치는 공정변수는 충전전압, 모재와 접합재 사이의 간격 및 접합재의 직경과 두께의 비(D/T비)로서 보고되었으며, Al/Steel 이종 금속 접합시 이들 공정변수가 접합부에 미치는 영향 및 최적의 공정변수 도출을 위한 연구는 시도되지 않았다. 따라서 본 연구는 전자기 펄스 용접기술을 이용한 Al/Steel 이종금속 접합 실험을 통하여 전자기 펄스용접의 적정성과 최적의 충전전압, 모재와 접합재 사이의 간격, D/T비를 도출하고자 한다. 전자기 펄스 용접 장치는 한국생산기술연구원과 웰메이트(주)에서 공동으로 개발한 $120{\mu}F$의 캐패시터 6개로 구성된 'W-MPW36'을 사용하였으며 이 장치의 최대충전전압과 최대접합용량은 각각 10kV, 36kJ이다. 접합재는 전기 전도율의 높은 Al 1070 파이프를 사용하였으며 모재는 기존 스틸 요크재인 SM45C 환봉을 사용하였다. 기보고된 연구를 통하여 코일과 접합재 사이의 간격이 좁을수록 높은 전자기력이 접합재에 작용하는 것을 확인하였으나 코일내 접합재와 모재 삽입 편의를 위하여 1mm로 설정하였다. 접합부의 품질 평가를 위하여 수압시험을 실시하였으며, 시험 후 접합부 단면을 주사전자현미경(SEM)을 이용하여 관찰하였다.

• Journal of Welding and Joining
• /
• v.16 no.2
• /
• pp.84-92
• /
• 1998

On this study, the variations of hardness and microstructure were observed at he spot-welded part of 5182 alminum alloy sheets with thickness of 1.2 mm. The hardness of spot-welded part of aluminum alloy indicated the lowest value at nugget center. Also, the position where fatigue crack exists was investigated by surveying microstructure of the spot-welded sections. Mean load-deformation diagrams were obtained from static tensile test. Fracture was occurred completely within 5 mm after transforming elastic into plastic area. Fatigue test was stopped when the specimens of fatigue test had the final displacement of 0.2mm and measured fatigue bending angle and crack length. This study utilized them, investigated the relations between fatigue bending angle and fatigue crack length and made a estimation of the fatigue fracture life of resistance spot welded part of 5182 aluminum alloy sheet. The relative equation o fatigue crack length and fatigue failure life can be represented by {TEX}$L_{C}${/TEX}=α{TEX}$N_{f}^ {β}${/TEX}.

• Journal of the Korean Society of Manufacturing Technology Engineers
• /
• v.19 no.6
• /
• pp.841-846
• /
• 2010

The present study examined the mechanical properties of the friction welding with hollow and solid shaft of SM45, of which the diameter is 25.2mm and 33mm. Friction welding was conducted at welding conditions of 2,000rpm, friction pressure of 50MPa, upset pressure of 70MPa, friction time of 0.4sec to 1.4sec by increasing 0.2sec, upset time of 2.0 sec including variable such as friction time are following. Under these conditions, a tensile test, a hardness test and a microstructure of weld interface were studied. The results were as follows : When the friction time was 1.0 seconds under the conditions, the maximum tensile strength of the friction weld happened to be 1,094MPa, which is 120% compared with the tensile strength of SM45C base metal. The upset length linearly increased as friction time increased. According to the hardness test, the hardness distribution of the weld interface was formed from 475Hv to 739Hv. HAZ(Heat Affected Zone) was formed from the weld interface to 2mm of SM45C.

• Journal of Advanced Marine Engineering and Technology
• /
• v.37 no.8
• /
• pp.877-885
• /
• 2013

A seawater pipe of the engine room in the ships is being surrounded with severely corrosive environments caused by fast flowing of the seawater, containing aggressive chloride ion and high conductivity etc.. Therefore, the leakage of the seawater from its pipe have been often occurred due to its local corrosion by aggressive chloride ions. Subsequently, its leakage area is usually welded by AC shielded metal arc welding with various electrodes. In this study, when the sea water pipe is welded with several types of electrodes such as E4301, E4311, E4313 and E4316, a difference of the corrosion resistance on the welding metal zones was investigated using an electrochemical method, observing microstructure, measuring polarization behaviors and hardness. The weld metal zone welded with E4313 electrode exhibited the lowest value of hardness compared to other weld metal zones. In addition, its zone indicated also the best corrosion resistance than those of other weld metal zones. Furthermore, all of the weld metal zones revealed a relatively better corrosion resistance than those of the base metal zones. and also showed higher hardness than the base metal zones.

• KSCE Journal of Civil and Environmental Engineering Research
• /
• v.7 no.1
• /
• pp.93-101
• /
• 1987

Residual stresses have remained around welding areas of a steel structure member after welding operation. The major causes to occur these residual stresses are the local heat due to a welding, the heat stresses due to a irregular and rapid cooling condition, the material and rigidity of a steel structure. Ultimatly, these residual stresses have been known to decrease a brittle fracture strength, a fatigue strength, a buckling strength, dynamic properties, and the corrosion resistance of the material. This paper deals with the residual stresses on a steel structure member through experimental studies. SWS 58 plates were welded by the method of X-groove type. These plates were layed on the heat treatment at four different temperatures; $350^{\circ}C$, $500^{\circ}C$, $650^{\circ}C$ and $800^{\circ}C$. The resulting residual Stresses were measured by hole drilling method, and the followings were obtained. The residual stresses on the vicinity of a welding point were relieved most effectively at the temperature of $650^{\circ}C$, and these stresses relieved completly when the ratio of a hole diamerter to a hole depth became unity. Hardness test shows that the higher value of hardness at the heat affected zone dropped to belower as the temperature went up from $350^{\circ}C$ to $800^{\circ}C$. The Welding input heats have not influenced the magnitude of residual stresses at the input heat range between above and below one forth than standard.

• Proceedings of the KWS Conference
• /
• 2006.10a
• /
• pp.187-189
• /
• 2006

최근 유연솔더에서 무연솔더로 전환함에 따라서 PCB의 도금이 솔더접합부의 각도에 미치는 영향이 중요하게 되었다. 현재 PCB 도금은 Sn, Au, OSP 등으로 다양하게 진행되고 있다. 그러나 PCB 도금이 솔더접합부의 강도에 미치는 영향에 대한 연구는 아직 미비하다. 따라서 본 연구에서는 PCB 도금(Sn, Au, OSP)이 무연솔더(Sn-3.0Ag-0.5Cu) 접합부의 초기 전단강도에 미치는 영향과 열사이클시험 후 솔더접합부의 전단강도에 미치는 영향에 대해서 연구하였다.