• 대한기계학회논문집A
• /
• 제34권1호
• /
• pp.85-90
• /
• 2010

자동차 후진기어용 축재는 단조재로서 그 형상은 복잡하고 열처리 및 가공공정이 어려울 뿐 아니라, 제품수명 저하 등의 문제점으로 인한 경제적 손실이 크다. 따라서 종전의 일체형 단조품을 캠 형상 부분만을 기존의 단조품(SF 45)으로 사용하고, 나머지 축 부분은 일반 기계구조용 탄소강재(SM 45C)로 대체를 위한 이종마찰용접을 적용하였다. 마찰용접 변수인 회전수, 마찰압력, 업셋압력, 가열시간, 업셋시간 등의 상호작용에 의한 용접품질과의 상관관계를 고찰하였으며, 최적조건에서 마찰용접을 한 후 용접재(as-welded)와 고주파 열처리를 시행한 후열처리재(PWHT)의 접합부 특성을 비교 고찰하였다. 이는 종전의 일체형 단조품에 비해 단조비용 절감, 피로수명향상, 기계가공에 따른 공정수 및 재료절감 등의 경제적 파급효과가 클 것으로 기대된다.

• Journal of Welding and Joining
• /
• 제4권2호
• /
• pp.47-52
• /
• 1986

Friction Welds are formed by the mechanisms of diffusion as well as mechanical inter-locking. The severe plastic flow at the interface by the forge action of the process brings the subsurface so close together that detection of any unbounded area becomes very difficult. No reliable method is available so fat to determine the weld quality nondestructively. The paper presents an attempt to determine weld strength quantitatively using the ultrasonic pulseecho method. The new approach calculates the coefficient of reflection based on measured amplitudes of the echoes. This coefficient provides a single quantitative measurement which involves both acoustic energy reflected at the welded interface as well as transmitted across the interface. As a result, it was known that the quantitative relationship between the coefficient and the weld strength (torsional strength) could be drawn.

• 대한용접접합학회:학술대회논문집
• /
• 대한용접접합학회 2006년 추계학술발표대회 개요집
• /
• pp.115-116
• /
• 2006

• 대한용접접합학회:학술대회논문집
• /
• 대한용접접합학회 2006년도 춘계 학술대회 개요집
• /
• pp.283-285
• /
• 2006

• 열처리공학회지
• /
• 제34권6호
• /
• pp.309-314
• /
• 2021

Due to the superior corrosion resistance and mechanical properties of TiAl alloy at high temperature, it has been utilized as a turbine wheel of a turbocharger. The dissimilar metallic bonding is usually applied to combine the TiAl turbine wheel with the SCM440 structural steel which is used as a driving shaft. In this study, the TiAl and SCM440 joint were fabricated by using a friction welding technique. During bonding process, to suppress the martensitic transformation and the formation of cracks, which might reduce a strength of the joints, Cu was used as an insert metal to relieve stress. As a result, the intermetallic compounds (IMCs) layer was observed at TiAl/Cu interface while no IMC formation was formed at SCM440/Cu interface. Since understanding of the IMCs effects on the mechanical performance of welded joint is also essential for ensuring the reliability and integrity of the turbocharger system, we estimated the nanohardness of welded joint region through nanoindentation. The relation between the microstructural feature and its mechanical property is discussed in detail.

• Journal of Welding and Joining
• /
• 제30권5호
• /
• pp.22-26
• /
• 2012

Butt-joints of A6061-T6 and AZ31 plates were successfully manufactured by using a friction stir welding method. Off-set free joints and off-set joints were fabricated to investigate the effect of the tool plunge position on the mechanical properties of the joints. Hardness test, tensile test and charpy impact test was performed to evaluate the mechanical properties of the joints. Off-set condition resulted in increase of mechanical properties of the joints. The variation of the hardness distribution in the SZ was also stabilized in the off-set condition. Tensile strength of the off-set joint was about 85% against to that of the AZ31 base metal. Impact absorption energy by Charpy-Impact-Test of the off-set joint also increased by almost 2 times against to that of the AZ31 base metal.

• 대한기계학회논문집A
• /
• 제41권3호
• /
• pp.219-224
• /
• 2017

본 연구는 수송기계 축 등에 이용되는 캠 형상 부분만을 기존의 단조품인 SF45와 축 부분은 일반기계구조용 탄소강재인 SM45C를 직경 20 mm를 이용하여 이종 마찰용접을 수행하였다. 최적조건을 규명하기 위해 인장시험 등 용접품질과의 상관관계를 고찰하였고, 또한 최적조건에서 마찰용접 후 열처리를 시행하여 용접재(As-welded)와 후열처리재(PWHT)에 대한 회전굽힘 피로시험을 시행하였다. 결과적으로 두 이종재가 강한 혼합으로 계면에서도 개재물 및 산화막이 플래시로 토출되어 양호한 접합상태임을 확인하였다. 더욱이 모재(SF45)와 후열처리재의 피로한도 각각 180 MPa, 250 MPa로 나타났다. 이는 후열처리재가 SF45 모재에 비해 약 40 %의 피로수명이 향상되었음을 확인하였다.

• 한국공작기계학회:학술대회논문집
• /
• 한국공작기계학회 1998년도 추계학술대회 논문집
• /
• pp.140-145
• /
• 1998

In this study, analysis for fatigue crack propagation behavior of interface and aroud interface under rotary bending stress. Though K values are nearly the same in around interface by BEM 2-D, fatigue crack propagated H.A.Z. Around Interface crack propagation speed is m=0.678 in H.A.Z by Paris' law. In this case(friction welded materials: STS304, SM15C), fatigue crack growth is considered SM15C metal microstructure and elastic flow from this result. Result is more metal microstructute dependence than stress dependence by analysis (BEM 3-D, BEM 2-D) and fatigue crack propagation

• 한국해양공학회지
• /
• 제19권2호
• /
• pp.53-59
• /
• 2005

The effect of pH on the corrosion characteristics in the dissimilar friction welded zone of IN713LC-SCM440 in the loaded torsional stress was studied. The corrosion experiment was performed for 120 hours on the specimens with five steps of pH. The surface corrosion pattern of the SCM440 area showed global corrosion and narrow pitting, which was caused by galvanic corrosion between friction welded IN713LC and SCM440, but corrosion did not proceeded from the IN713LC area. The average relative electrode potential gradually tends to decrease with the elapse of the immersion time in the acidity area. The average corrosion current also gradually tend to decrease The corrosion rate showed a larger value when the average relative electrode potential was higher and the average relative current was lower. The corrosion rate showed a larger value when the average relative electrode potential was higher in the acidity area, and it showed large when the average relative electrode potential was lower in the alkalinity area.

• 한국자동차공학회논문집
• /
• 제10권2호
• /
• pp.186-192
• /
• 2002

The fatigue crack propagation characteristics were investigated on dissimilar friction weld of two kind of heat-resisting steels (STR3 and STR35) commonly used in valve materials for vehicles. A small circular artificial defect was machined to induce fatigue crack at bonded line, heat affected zone and base metal of the weld on the surface of the specimens. From the results of the experiment, the fatigue limits of the materials STR3 and STR35 were obtained to be 429.0MPa and 409.4MPa respectably. The STR35 base metal and 1.0mm HAZ specimens showed 190% and 82% higher fatigue life than STR3 base metal. And the fatigue life of 1.0mm HAZ specimen was shown 99% on STR3 and 29% on STR35 higher than that of their base metal. But the fatigue life of weld interface specimen was shown 18% on STR3 and 72% on STR35 lower than that of their base metal because of the weld interface separation.