• 제목/요약/키워드: Joining behavior

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6mm$^{t}$ 조선용 Primer코팅강판의 $CO_2$ 레이저 용접성 (II) - 레이저 용접현상의 동적거동과 기공 및 증발입자의 조성 - (The Weldability of 6mm$^{t}$ Primer-coated Steel for Shipbuilding Using $CO_2$ Laser (II) - Dynamic Behavior of Laser Welding Phenomenon and composition of porosity and vaporized-particle -)

  • 김종도;박현준;이종봉
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2003년도 춘계학술발표대회 개요집
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    • pp.234-237
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    • 2003
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무전해 니켈 도금액 pH 변화에 따른 ENIG/Sn-Ag-Cu솔더 접합부의 취성파괴 특성 (Brittle Fracture Behavior of ENIG/Sn-Ag-Cu Solder Joint with pH of Ni-P Electroless Plating Solution)

  • 서원일;이태익;김영호;유세훈
    • 마이크로전자및패키징학회지
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    • 제27권3호
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    • pp.29-34
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    • 2020
  • 본 연구에서는 무전해 니켈 도금액 pH 변화에 따른 electroless nickel immersion gold (ENIG)/Sn-3.0wt.%Ag-0.5wt.%Cu(SAC305) 솔더 접합부 취성 파괴 거동에 대하여 평가하였다. ENIG 표면처리를 위한 무전해 니켈 도금액의 pH는 4.0에서 5.5로 변화 시켰다. 무전해 니켈 도금 후 Ni-P 표면 관찰 결과, 도금액의 pH가 낮아질수록 Ni-P 층 nodule 표면에 핀홀이 증가하였다. 솔더링 후 접합부 계면에서는 (Cu,Ni)6Sn5 금속간화합물이 형성되었으며, 무전해 니켈 도금액의 pH가 증가할수록 솔더접합부의 계면 금속간화합물의 두께는 증가하였다. 고속전단 시험을 통하여 ENIG/SAC305 솔더 접합부의 취성파괴 거동을 확인하였으며, 무전해 니켈 도금액의 pH가 증가할수록 솔더접합부의 전단강도는 감소하는 경향을 보였다. 또한, 솔더 접합부의 취성 파괴율은 pH가 5일 때 가장 높은 값을 보였다.

Ni-Cr-Fe 및 Ni-Fe-Cr-Mo계 합금의 용접부 균열특성에 관한 연구 Part I : 용착금속의 응고균열 (A Study on the Cracking Behavior in the Welds of Ni-Cr-Fe and Ni-Fe-Cr-Mo Alloys Part I : Solidification Cracking in the Fusion Zone)

  • 김희봉;이창희
    • Journal of Welding and Joining
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    • 제15권4호
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    • pp.78-89
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    • 1997
  • This study has evaluated the weld metal solidification cracking behavior of several Ni base superalloys (Incoloy 825, Inconel 718 and Inconel 600). Austenitic stainless steels(304, 310S) were also included for comparison. In addition, a possible mechanism of solidification cracking in the fusion zone was suggested based on the extensive microstructural examinations with SEM, EDAX, TEM, SADP and AEM. The solidification cracking resistance of Ni base superalloys was found to be far inferior to that of austenitic stainless steels. The solidification cracking of Incoloy 825 and Inconel 718 was believel to be closely related with the Laves-austenite (Ti rich in 825 and Nb rich in 718) and MC-austenite eutectic phases formed along the grain boundaries during solidification. Cracking in Inconel 600 was always found along the grain boundaries which were enriched with Ti and P. Further, solidifidcation cracking resistance was dependent not only upon the type of love melting phases but also on the amount of the phases along the solidification grain boundaries.

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오스테나이트계 스테인리스강 레이저 용접부의 응고균열 거동 (Part 1) - 레이저 용접용 Varestraint 시험 시스템을 이용한 응고균열 민감도 평가 - (Solidification Cracking Behavior in Austenitic Stainless Steel Laser Welds (Part 1) - Evaluation of Solidification Cracking Susceptibility by Laser Beam Welding Varestraint Test -)

  • 천은준;이수진;서정;강남현
    • Journal of Welding and Joining
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    • 제34권5호
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    • pp.54-60
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    • 2016
  • In order to quantitatively evaluate the solidification cracking susceptibility in laser welds of three types of austenitic stainless steels (type 310: A mode, type 316-A: AF mode, type 316-B: FA mode solidifications), the laser beam welding (LBW) transverse-Varestraint tests consisted of multi-mode fiber laser, welding robot and hydraulic pressure system were performed. As the welding speed increased from 1.67 to 40.0 mm/s, the solidification brittle temperature range (BTR) of laser welds for type 316 stainless steels enlarged (316-A: from 37 to 46 K, 316-B: from 14 to 40 K), while the BTR for type 310 stainless steel reduced from 146 to 120 K. In other words, it founds that solidification cracking susceptibility could not be simply mitigated through application of LBW process, and the BTR variation behavior is quite different upon solidification mode of austenitic stainless steels.

TMCP 고장력강 용접부의 피로 특성에 관한 연구 (Fatigue properties of welded joints for TMCP steels)

  • 임채범;권영각;엄기원
    • Journal of Welding and Joining
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    • 제8권2호
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    • pp.40-52
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    • 1990
  • Fatigue behavior of the AH, DH and EH grade TMCP(Thermo-Mechanical Control Process) steels was studied. High cycle and low cycle fatigue tests were carried out for the weldment and base metal of each steel. The results showed that the fatigue limit at 2 * $10^6$ cycles was 33 to 37 kg/$mm^2$ for the base metal and 30 to 34 kg/$mm^2$ for the weldment. The ratio of fatigue limit to tensile strength for TMCP steels was 0.65 to 0.71, which was a value close to the upper limit for the ordinary steels. It was also found that the high cycle fatigue behavior of TMCP steels could be affected by the microstructures of base metal. It will be necessary to have fine structure for TMCP steels to increase the fatigue resistance. In low cycle fatigue test, the fatigue lifetime of AH and DH steels accorded well with the ASME best fit curve, while that of EH steel was considerably lower than the fatigue lifetime of the other steels. Fatigue resistance of the weldment made by high heat input(180kJ/cm) welding was not lower than that made by low heat input(80kJ/cm) welding in case of high cycle fatigue, but the high heat input welding decreased the fatigue resistance in case of low cycle fatigue.

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