• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.8
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• pp.751-758
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• 2009

Failure strengths of composite single-lap adhesive joints were investigated with various parameters such as manufacturing method, overlap length and adherend thickness. A total of 335 single-lap joint specimens were tested under tension. Specimens were fabricated with 4 different manufacturing processes; cocuring without and with adhesive, secondary bonding and co-bonding. Each manufacturing process has 5 different overlap lengths and 4 different thicknesses, respectively. As expected, failure strength is higher in thicker adherend joints and lower in larger overlap length specimens. Interesting result is that the secondary bonded joints show the higher strength than the cobonded and cocured joints with adhesive, and give close or even higher strength compared with non-adhesive cocured case.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.4 no.2
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• pp.133-142
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• 1984

With the weld-joined compact tension specimens compared with each other, that is, transverse and lengthwise about the crack propagation direction, high and low in the input heat level, same as and lower than the base metal in the strength of weld material, the fatigue test were performed. With these data, the log-log curves between the fatigue crack propagation rate ${\frac{da}{dN}}$ and the transition range of the stress intensity factor ${\Delta}K$ ahead the crack tip were drawed. These curves were compared and estimated among each compared specimens, among each zones, that is, the base metal, the heat-affected metal and the weld-mixed metal, and between this study and the past studies. Basically, Little difference in the slope of the $da/dN-{\Delta}K$ relation was showed in all the welded directions, all the input heat levels and all the zones. But, First, to comparison with in the past studies about the base metals, it was showed that da/dN started in the much later rate, increased faster and stoped in the little faster rate. Second, it was showed that, near the time the crack's going from the heat-affected zone to the weld-mixed metal da/dN decreased a little for a while. Third, in the lengthwise weld compared with the transverse weld, in the high input heat weld compared with the low input heat weld in the case used the weld material of the same strength as the base metal, in the opposite case in the case used the one of the lower strength than the base metal, in the case used the weld material of the same strength as compared with the lower strength than the base metal beside the high input heat and the lengthwise weld, it was showed that the crack occured earlier in lower ${\Delta}K$ and later da/dN, the curves went with the same slope. Forth, in the lengthwise weld compared with the transverse weld in the low input heat weld, in the low input heat weld compared with the high input heat weld, it was showed that da/dN went with the lower level.

• Transactions of the Korean Society of Machine Tool Engineers
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• v.18 no.2
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• pp.221-227
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• 2009

The study of the solidification process of welded metal is carried out using the finite element method, which is the basic study for optimal design. In the analysis of temperature, the welded zone is cooled as the result of heat conduction to the base metal and heat transfer to the circumference. In the early phase of the temperature in base metal zone is little changed. But after the rise in temperature the whole area is cooled gradually and uniformly with the lapse of 10 seconds, and a temperature change is hardly occurred in the radial direction but in the axial direction.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.8
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• pp.65-70
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• 2002

The brazing of duplex stainless steels which is an essential process for rocket engine manufacturing has been investigated on bonding phenomena and shear strength. The UNS32550 was used for base metal, and the MBF-50 was used for insert metal. Brazing was carried out under the various conditions (brazing temperature : 1473K, 1498K, holding time : 0, 0.3, 0.9, 1.8 ks). There were various phases in the joint because of reaction between liquid insert metal and base metal, In the early stage, BN is formed in the bonded interlayer and base metal near the bonded layer. Cr nitride is formed in the bonded interlayer. The amount of BN and Cr nitride decrease with the increase of holding time. Superior shear strength of 550MPa is obtained by restraining the formation of nitride.

• Proceedings of the KWS Conference
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• 2004.05a
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• pp.48-50
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• 2004

TLP 접합 공정에서 모재와 삽입금속 사이에서의 확산을 통하여 액상 삽입금속은 고온에서 등온으로 유지 시 등온 응고된다. D.S.Duvall은 느린 가열시 매우 빠른 속도로 가열 시 보다 낮은 온도에서 dissolution이 완료되고 응고가 발생할 것으로 예상하였다. (중략)

• Journal of the korean Society of Automotive Engineers
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• v.12 no.4
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• pp.28-34
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• 1990

저항용접은 에리후 톰슨(Elihu Thomson)이 1877년에 처음 개발하였으나, 1920년 이후부터 보급이 시작되어 1935년경부터 수요가 증대되었는데, 초기에는 Butt용접을 이용한 전선접합과 넓게는 레일의 용접에까지 보급되었다. 스파타는 전극이 하강하기 이전에 전류가 흐를 때, 용접 모재에 충분한 가압이 이루어지지 않은 상태에서 전류가 통하므로 발생하는 초기 스파타와, 전극이 상승할 시에 전류가 끊어지지 않은 상태일 때 발생되는 통전후기 스파타가 있는데 이때 용접모재는 불량이 된다. 이와 같은 불량을 감소시키기 위한 일환으로 용접작업 후의 자료관리를 시행함으로써 불량품 해소에 응용하고자 한다.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.21 no.5
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• pp.515-524
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• 2008

The ultimate behavior of high-tension bolted joints with various plate thickness and bolt size is investigated using nonlinear F.E. analysis and experimental study. The relation with sliding load, bolt deformation, and failure modes are presented based on plate thickness and bolt size. Three kinds of the bolt diameter(M20, M22, M24) and five types of the steel plates (l2mm, 16mm, 20mm, 30mm, 40mm) are considered for the ultimate behavior of the bolted joints. The numerical model, constructed by commercial F.E. program, ABAQUS, of ultimate behavior of bolted joints is introduced and verified by experimental results. The force-displacement and force-axial strain relations are measured and compared with the results by 3D finite element analysis.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2011.05a
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• pp.187-187
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• 2011

지르코니아 ($ZrO_2$) 표면에 금속 (Au)으로 표면 코팅한 후 Ti-6Al-4V와 진공 브레이징 접합을 행하였다. 표면에 코팅한 Au 층의 영향을 비교 분석하기 위하여 Au를 코팅하지 않은 지르코니아도 모재로 사용하였다. 접합소재로는 Ag-Cu-Ti계 active filler를 사용하였다. $ZrO_2$/Ti-6Al-4V 브레이징 결과, active filler는 양측 모재 표면에 wetting 되었으며, Ti-6Al-4V 내부로 filler 확산으로 인하여 두 모재의 direct joint가 관찰되었다. 접합 계면 사이에 접합부 결함은 관찰되지 않았다.

• Proceedings of the KWS Conference
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• 1997.10a
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• pp.40-42
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• 1997

1)X65배관의 심 및 원주용접 부분과 X42배관의 원주용접 부분에 대하여, 노치 위치 및 시험온도 변화에 따른 충격 및 파뢰인성 변화를 비교, 분석하였다. 2) 모든 경우에 용착금속부에 대한 충격 및 파괴인성이 가장 취약하게 나타났다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.619-622
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• 2009

INCONEL 718합금은 상온, 고온 및 저온환경에서 기계적 특성이 아주 우수하다. 상온에서의 모재 강도는 약 900MPa이며, 열처리 후 시효경화처리에 의해 강도가 약 1300MPa까지 증가한다. 이러한 INCONEL 718합금의 기계적 특성은 시험결과에서도 유사한 값을 나타내었고, GTAW 용접부의 상온 기계적 특성도 모재보다 우수한 강도를 나타내었다. 또한 저온에서의 기계적 특성은 모든 시험조건에서 상온보다 높은 강도를 나타내었으며, 열처리 모재시편과 용접시편은 1400MPa에 달하는 고강도를 나타내었다. 이러한 결과를 바탕으로 INCONEL 718합금의 저온 기계적 특성이 우수한 것을 증명하였고, 용접성 또한 모재의 특성과 같이 상온 및 저온 특성이 우수한 것을 알 수 있었다. INCONEL 718 합금과 STS 316L의 이종접합의 경우에도 $-100^{\circ}C$환경의 인장강도가 상온보다 300MPa 이상 증가하는 것을 알 수 있었다. 따라서, INCONEL 718합금은 $100^{\circ}C$이하부터 일정온도까지는 기계적 특성이 계속 증가 할 것으로 사료되며, 극저온 고압 상태로 공급되는 산화제 배관 제작에 적합한 소재로 판단된다.