• 제목/요약/키워드: high Heat Input Welding

검색결과 187건 처리시간 0.022초

용접(鎔接)이음한 구조강(構造鋼)의 소인장시험편(小引張試驗片)에서의 피로구열진전거동(疲勞龜裂進展擧動) (용접방향(鎔接方向), 입열량(入熱量), 용접재료(鎔接材料)의 강도(强度) 등이 다를 때) (The Propagation Behaviour of the Fatigue Crack in the Compact Tension Specimens of the Welded Structural Steels (On according to the difference of the welding direction, the input heat level, the strength of weld material and so on))

  • 장동일;정영화
    • 대한토목학회논문집
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    • 제4권2호
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    • pp.133-142
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    • 1984
  • 횡방향(橫方向)과 종방향(縱方向), 대입열용접(大入熱鎔接)과 소입열용접(小入熱鎔接), 모재(母材)와 같은 강도(强度)의 용접재료(鎔接材料) 사용(使用)과 모재(母材)보다 낮은 강도(强度)의 용접재료(鎔接材料) 사용(使用) 등으로 서로 비교되는 용접(鎔接)이음의 소인장시험편(小引張試驗片)을 만들어서 피로시험(疲勞試驗)을 행하여 피로구열(疲勞龜裂) 진전속도(進展速度) ${\frac{da}{dN}}$와 구열선단(龜裂先端) 부근의 응력확대계수(應力擴大係數)의 변동범위(變動範圍) ${\Delta}K$와의 관계곡선(關係曲線)을 그려서 비교시험간(比較試驗間)의 모재(母材), 열영향부(熱影響部) 및 용착금속부(鎔着金屬部)로 구분, 혹은 지금까지의 연구자료(硏究資料) 등과 비교검토하였다. 이 결과, 다음과 같은 현상들을 알 수 있었다. 기본적(基本的)으로, 용접방향(鎔接方向), 용접입열량(鎔接入熱量), 용접재료(鎔接材料)의 강도(强度), 혹은 모재(母材), 열영향부(熱影響部) 및 용착금속부(鎔着金屬部)의 구분 등에 따라 ${\frac{da}{dN}}-{\Delta}K$관계에 큰 차이가 없었다. 다만, 첫째, 소재(素材)에 대한 경우에 비해 대개 처음은 같은 ${\Delta}K$에서 ${\frac{da}{dN}}$가 상당히 늦다가 점차 증가하여 중간쯤에서 같아진 후 끝 부분에서 같은 ${\Delta}K$에서${\frac{da}{dN}}$가 다소 빨라짐을 알 수 있었다. 둘째, 열영향부(熱影響部)에서 용접금속부(鎔接金屬部)로 진전(進展)하면서 ${\frac{da}{dN}}$가 다소 늦어지는 것을 알 수 있었다. 셋째, 용접방향(鎔接方向)과 구열방향(龜裂方向)이 평행인 경우가 직각인 경우에 비해, 모재(母材)와 같은 용접재료(鎔接材料)를 쓴 경우 소입열용접(小入熱鎔接)인 경우가 대입열용접(大入熱鎔接)인 경우에 비해, 모재(母材)보다 낮은 용접재료(鎔接材料)를 쓴 경우 대입열용접(大入熱鎔接)인 경우가 소입열용접(小入熱鎔接)인 경우에 비해, 대입열(大入熱)의 평행용접(鎔接)의 경우를 제외한 모든 용접(鎔接)에서 모재(母材)와 같은 강도(强度)의 용접재료(鎔接材料)를 쓴 경우가 모재(母材)보다 낮은 강도(强度)의 용접재료(鎔接材料)를 쓴 경우에 비해 ${\Delta}K$가 낮은 시기(時期)에 일찍 저속(低速)으로 구열(龜裂)이 시작되어 ${\Delta}K$의 큰 증가없이 ${\frac{da}{dN}}$가 빠르게 증가한 다음 다른 경우와 같은 성상(性狀)으로 진전됨을 알 수 있었다. 넷째, 소입열용접(小入熱鎔接)의 경우 평행용접(鎔接)이 직각용접(鎔接)에 비해, 소입열용접(小入熱鎔接)이 대입열용접(大入熱鎔接)에 비해 같은 ${\Delta}K$에서 ${\frac{da}{dN}}$가 다소 늦은 것을 알 수 있었다.

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Fatigue Life of the Repair TIG Welded Hastelloy X Superalloy

  • SIHOTANG, Restu;CHOI, Sang-Kyu;PARK, Sung-Sang;BAEK, Eung-Ryul
    • Journal of Welding and Joining
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    • 제33권5호
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    • pp.26-30
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    • 2015
  • Hastelloy X in this study was applied in jet engine F-15 air fighter as shroud to isolate the engine from outer skin. After 15 years operation at elevated temperature the mechanical properties decreased gradually due to the precipitation of continues second phases in the grain boundaries and precipitated inside the grain. The crack happened at the edge of the shroud due to the thermal and mechanical stress from jet engine. Selective TEM analysis found that the grain boundaries consist of $M_{23}C_6$ carbide, $M_6$ Ccarbide and small percentage of sigma(${\sigma}$) phase. Furthermore, it was confirmed the nano size of ${\sigma}$ and miu (${\mu}$) phase inside the grain. In this study, it was investigated the microstructure of the degraded shroud component and HAZ of repair welded shroud. In the HAZ, it was observed the dissolution of the $M_{23}C_6$ carbides and smaller precipitates, the migration of the undissolved larger $M_{23}C_6$ carbide and $M_6$ Ccarbide. It is also observed the liquation due to the simply melt of the segregated precipitates in the grain boundaries. Interestingly, the segregated second phases which simply melt in the grain boundaries more easily happened at higher heat input welding condition. High temperature tensile test was done at $300^{\circ}C$, $700^{\circ}C$ and $900^{\circ}C$. It was obtained that the toughness of welded sample is lower compare to the non-welded sample. The solution heat treatment at $1170^{\circ}C$ for 5 minutes was suggested to obtain a better mechanical properties of the shroud. The high cycle fatigue number of the repair welded shroud shows a much lower compare to the shroud. In addition, the high cycle fatigue number at room temperature after solution heat treatment was almost double compare to the before solution heat treatment under 420-500MPa stress amplitude. However, the high cycle fatigue number of repaired welded sample was shown a much lower compare to the non- welded shroud and solution treated shroud. One of the main reasons to decrease the tensile strength and the high cycle fatigue properties of the repair welded shroud is the formation of the liquid phase in HAZ.

SP-SSRT법에 의한 TMCP강 용접부의 응력부식균열 평가에 관한 연구 (A Study on the Stress Corrosion Cracking Evaluation for Weld Joint of TMCP steel by SP-SSRT Method)

  • 유효선;정희돈;정세희
    • Journal of Welding and Joining
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    • 제15권1호
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    • pp.46-54
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    • 1997
  • The object of this paper is to evaluate SCC(stress corrosion cracking) susceptibility for parent metal and bond line region of weld joints which have the various weld heat input condtions in TMCP(thermo-mechanical control process) steel by SP-SSRT(small punch-slow strain rate test) method. And the SCC test results of TMCP steel are compared with those of the conventional HT50 steel which has te almost same tensile strength level like TMCP steel. The loading rate used was $3\times10^{-4}$mm/min and the corrosive environment was synthetic sea water. According to the test results, in the case of parent metal, TMCP steel showed higher SCC susceptibility than HT50 steel because of the high plastic strain level of ferrite microstructure obtained by accelerated cooling. And in the case of bond line, the both TMCP steel and HT50 steel showed low load-displacement behaviors and higher SCC susceptibility above 0.6. These results may be caused by theembrittled martensite structure on HT50 steel and by the coarsened grain and the proeutectoid ferrite structure obtained by the impart of accelerated cooling effect on TMCP steel.

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극후판 EH40 TMCP강재 Tandem EGW 용접부의 잔류응력 해석 (Numerical Analysis of Welding Residual Stresses for Ultra-Thick Plate of EH40 Steel Joined by Tandem EGW)

  • 황세윤;이장현;김병종;양용식
    • 대한조선학회논문집
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    • 제47권6호
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    • pp.821-830
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    • 2010
  • Deck plates and hatch coming of large container carrier and offshore structures are joined by ultra-thick plates whose thickness is more than 60mm. Traditionally FCAW has been used to join the thick plates in butt joint. However, FCAW has been replaced with EGW since the welding efficiency of EGW is higher than that of FCAW. Tandem EGW using two electrodes has been applied to vertical position welding by several shipyards. EGW requires one or two layers of bead whereas FCAW requires more than 20 layers of weld bead in thick welding. However, high welding residual stresses are generated by EGW since it uses higher heat input than FCAW. In the present study, a finite element model is suggested to predict the residual stresses induced by the tandem EGW. Butt specimen of EH40 TMCP shipbuilding steel plates vertical welding was modeled by a three-dimensional model. Residual stresses were measured by X-ray diffraction method and to verify the numerical result. The results show a good agreement with experimental result.

대입열용접 열영향부의 조직과 인성 (HAZ Microstructure and Toughness in High Heat Input Welding)

  • 방국수;이종봉;장래웅
    • Journal of Welding and Joining
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    • 제10권1호
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    • pp.12-19
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    • 1992
  • 용접능률의 향상을 위한 대입열용접법의 적용은 과도한 입열량으로 인하여 용접부의 인성이 저 하한다는 점에서 그 적용에 주의를 요한다. 본 보에서는 대입열용접시 열영향부의 인성 저하의 원인과 그 대책을 강재의 측면에서 검토하였다. 고장력강을 용접하면 입열량이 증가함에 따라 오스테나이트 결정립이 조대화되고 상부 베이나이트와 도상 마르텐사이트가 생성되어 인성이 저하한다. 그 대책으로서는 용접 열싸이클과정중 안정한 질화물, 산화물등을 모재에 미세분산시켜 오스테나이트 결정립 성장을 억제하고, 페라이트, 펄라이트 변태를 촉진시킨다. 이러한 석출물의 형성을 위해서는 주로 Ti, Ca, REM, B등의 합금원소가 이용된다. 소입성이 높은 주질고장력 강에서는 석출물의 분산에 의한 페라이트의 변태 촉진 보다는 Mn, Ni, Cr, Mo, V등의 합금원 소를 첨가하여 소입성을 높여 인성이 우수한 하부 베이나이트 조직을 형성하든가, 탄소량을 저 감시켜 도상 마르텐사이트의 생성을 억제하므로서 인성을 확보한다. 현재 국내에서 제조되고 있는 대입열용접용강중 인장강도 50kgf/mm$^{2}$급강은 기본적으로 용접부 인성이 우수한 TMCP법으로 제조되며, Ti등을 첨가하여 석출물의 효과를 이용하고 N을 억제하여 기지의 인 성을 향상시키는 등의 방법을 병용하고 있다. 인장강도 60kgf/mm$^{2}$ 급강은 조질처리에 의하여 제조되며, 50kgf/mm$^{2}$급강과 같이 Ti, B등의 첨가에 의한 석출물의 효과를 이용 하고 있다.

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델타스폿용접을 이용한 이종소재 웰드본딩공정 시 표면 거칠기 부여 가공방법의 영향 (Effect of Surface Roughness on Weld-bonding Process using Heterogeneous Materials)

  • 김영현;김재웅;김지선;김영곤;표창민
    • 한국기계가공학회지
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    • 제19권11호
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    • pp.102-108
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    • 2020
  • The demand for lightweight materials and high-strength steel has rapidly increased to help reduce the weight of a vehicle body; it improves the fuel efficiency of automobiles and provides passenger safety. Additionally, as the material becomes thinner, the demand for its resistance against corrosion becomes higher. Hence, the application of the surface-treated steel sheet has surged rapidly. In this study, a weld bonding experiment using a delta spot welding machine is performed on a thin sheet of a different material (Al6061-T6/GA440). The thickness of the material was kept at 1 mm to reduce the weight of the automobile body parts. Additionally, the purpose of this study is to control the heat input by applying the welding conditions of a multi-stage pressure pattern to improve corrosion resistance shear strength. The analysis of nugget diameter measurement, shear tensile test, and salt spray test was performed to achieve the aim.

$CO_2$ 레이저를 이용한 GTD111DS 초합금 용접부의 미세조직과 기계적 성질 (Microstructures and Mechanical Properties of GTD 111DS Welds by $CO_2$ Laser Welding)

  • 이택운;양성호;김상훈
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2009년 추계학술발표대회
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    • pp.108-108
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    • 2009
  • 니켈기지의 석출강화 초내열합금은 가스터빈의 고온부 부품 제조에 널리 사용되고 있다. 장시간 동안 부품의 강성 유지와 구조적 안정성을 확보하기 위해서는 니켈기지의 합금에 감마프라임 생성을 위한 원소를 첨가하는데 이에 따른 용접성의 저하 때문에 보통 초합금의 용접은 고온에서 수행하게 된다. 그러나 레이저용접의 경우는 용접변수 및 입열제어가 용이해 상온에서 초합금의 용접이 가능한 장점이 있다. 본 연구에서는 일반적인 재료로 연성이 좋은 STS304 판재와 실제 블레이드의 재료로 사용되는 니켈계 석출강화 합금인 GTD 111DS 모재에 $CO_2$ 레이저를 이용하여 용접을 실시하였고 적용파우더와 파워, 용접속도 및 파우더 공급량 등을 달리 하였다. STS304 판재 사용시 Rene 80과 IN 625 파우더 모두 용접부에서 균열이 발생하지 않았다. 그러나 GTD 111DS 모재의 경우 IN 625 파우더에서는 결함이 없었으나 Rene 80 파우더를 사용시에는 용접부에 균열이 발생하였다. IN 625 파우더는 모재보다 기계적 성질이 떨어지는 문제가 있으나 Rene 80은 모재와 동등 이상의 기계적 성질을 보유하고 있기 때문에 Rene 80 의 적용을 위해 균열이 발생하지 않는 용접변수의 제어를 시도하였다. 용접변수의 조정 결과 레이저 파워와 파우더 공급량을 낮추고 용접속도를 높여 균열이 발생하지 않는 최적의 용접변수를 설정할 수 있었다. 최적화된 용접변수를 적용, 용접한 시편의 인장값을 보면 GTD 111DS 모재에 Rene 80 파우더로 용접된 시편의 인장강도가 상온/고온($760^{\circ}C$)의 조건에서 각각 GTD 111DS 모재의 인장강도 보다 높은 값을 나타내었다.

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하이브리드 방식 (CNC+Laser)을 이용한 폴리머용접공정 (Hybrid (CNC+Laser) process for polymer welding)

  • 유종기;이춘우;김순동;최해운;신현명
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2009년 추계학술발표대회
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    • pp.4-4
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    • 2009
  • Polycarbonate (PC) and Acrylonitrile Butadiene Styrene (ABS) was welded through a combination of a diode laser and CNC. Laser beam passed the transparent PC and was absorbed in an opaque ABS. Polymers were melted and welded by absorbed and conducted heat. Experiments were carried out by varying working distance from 44mm to 50mm for the focus spot diameter control, laser input power from 10W to 25W, and scanning speed from 100 to 400mm/min. The weld bead size and the specimen cross-section were analyzed, and tensile results were presented through the joint force measurement. With focus distance at 48mm, laser power with 20W, and welding speed at 300mm/min, experimental results showed the best welding quality which bead size was 3.75mm and the shear strength was $22.8N/mm^2$. Considering tensile strength of ABS is $43N/mm^2$, shear strength was sufficient to hold two materials. A single process was possible in CNC machining processes, surface processing, hole machining and welding. As a result, the process cycle time was reduced to 25%. Compared to a typical process, specimens were fabricated in a single process, with high precision. By combining two operations processes developed process gained 50% more efficiency.

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인장전단시험을 이용한 TRIP1180강의 계면파단특성 평가 (Evaluation of Resistance Spot Weld Interfacial Fractures in Tensile-Shear Tests of TRIP 1180 Steels)

  • 박상순;최영민;남대근;김영석;유지훈;박영도
    • Journal of Welding and Joining
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    • 제26권6호
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    • pp.81-91
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    • 2008
  • The weldability of resistance spot welding of TRIP1180 steels for automobile components investigated enhance in order to achieve understanding of weld fracture during tensile-shear strength (TSS) test. The main failure modes for spot welds of TRIP1180 steels were nugget pullout and interfacial fracture. The peak load to cause a weld interfacial failure was found to be related to fracture toughness of the weld and the weld diameter. Although interfacial fracture occurred in the spot welded samples, the load-carrying capacity of the weld was high and not significantly affected by the fracture mode. Substantial part of the weld exhibits the characteristic dimple (or elongated dimple) fractures on interfacial fractured surface also, dimple fracture areas were drawmatically increased with heat input which is propotional to the applied weld current. In spite of the high hardness values associated with the martensite microstructures due to high cooling rate. The high load-carrying ability of the weld is directly associated with the area of ductile fracture occurred in weld. Therefore, the judgment of the quality of resistance spot welds in TRIP1180 steels, the load-carrying capacity of the weld should be considered as an important factor than fracture mode.

HSLA-100강 및 HY-100강의 응력제거처리 균열에 관한 연구 (A Study on the Stress Relief Cracking of HSLA-100 and HY-100 steels)

  • 박태원;심인옥;김영우;강정윤
    • Journal of Welding and Joining
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    • 제14권3호
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    • pp.48-57
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    • 1996
  • A study was made to examine the characteristics of base metal and stress relief cracking(SRC) of heat affected zone(HAZ) for HY-100 and Cu-bearing HSLA-100 steels. The Gleeble thermal/mechanical simulator was used to simulate the SRC/HAZ. The details of mechanical properties of base plate and SRC tested specimens were studied by impact test, optical microscopy and scanning electron microscopy. The specimens were aged at $650^{\circ}C$ for HSLA-100 steel and at $660^{\circ}C$ for HY-100 steel and thermal cycled from $1350^{\circ}C$ to $25^{\circ}C$ with a cooling time of $\Delta$t_${800^{circ}C/500^{circ}C}$=21sec. corresponds to the heat input of 30kJ/cm. The thermal cycled specimens were stressed to a predetermined level of 248~600MPa and then reheated to the stress relief temperatures of $570~620^{\circ}C$. The time to failure$(t_f)$ at a given stress level was used as a measure of SRC susceptibility. The strength, elongation and impact toughness of base plate were greater in HSLA-100 steel than in HY-100 steel. The time to failure was decreased with increasing temperature and/or stress. HSLA-100 steel was more susceptible to stress relief cracking than HY-100 steel under same conditions. It is thought to be resulted from the precipitation of $\varepsilon$-Cu phase by dynamic self diffusion of solute atoms. By the precipitation of $\varepsilon$-Cu phase, the differential strengthening of grain interior relative to grain boundary may be greater in the Cu-bearing HSLA-100 steel than in HY-100 steel. Therefore, greater strain concentration at grain boundary of HSLA-100 steel results in the increased SRC susceptibility. The activation energies for SRC of HSLA-100 steel are 103.9kcal/mal for 387MPa and 87.6kcal/mol for 437MPa and that of HY-100 steel is 129.2kcal/mol for 437MPa.

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