• 제목/요약/키워드: Welding tip

검색결과 191건 처리시간 0.028초

용융 Zn 합금에서 Fe합금의 PTA 오버레이 용접 금속간 상의 형성과 진행 (Formation and Progression of Intermetallic phase on Iron Base Alloy PTA weld overlay in Molten Zn Alloys)

  • ;백응률
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2009년 추계학술발표대회
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    • pp.95-95
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    • 2009
  • Zinc coatings provide the most effective and economical way of protecting steel against corrosion. There are three types of galvanizing lines typically used in production line in galvanizing industries,Galvanize (GI) coating (Zn-0.1-0.3%Al), Galfan coating (Zn-5%Al), Galvalume(GL) coating (45%Zn-Al). In continuous Galvanizing lines, the immersed bath hardware (e.g. bearings, sink, stabilizer, and corrector rolls, and also support roll arms and snout tip) are subjected to corrosion and wear failure. Understanding the reaction of these materials with the molten Zn alloy is becomes scientific and commercial interest. To investigate the reaction with molten Zn alloys, static immersion test performed for 4, 8, 16, and 24 Hr. Two different baths used for the static immersion, which are molten Zn and molten Zn-55%Al. Microstructures characterization of each of the materials and intermetallic layer formed in the reaction zone was performed using optical microscope, SEM and EDS. The thickness of the reaction layer is examined using image analysis to determine the kinetics of the reaction. The phase dominated by two distinct phase which are eutectic carbide and matrix. The morphology of the intermetallic phase formed by molten Zn is discrete phase showing high dissolution of the material, and the intermetallic phase formed by Zn-55wt%Al is continuous. Aluminum reacts readily with the materials compare to Zinc, forming iron aluminide intermetallic layer ($Fe_2Al_5$) at the interface and leaving zinc behind.

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용접열영향부 충격시험편 노치 위치에 따른 파괴거동 (Failure Behaviors Depending on the Notch Location of the Impact Test Specimens on the HAZ)

  • 장윤찬;홍재근;박지홍;김동욱;이영석
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.706-711
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    • 2007
  • Numerical studies were performed to examine the effects of notch location of impact specimens on the failure behavior of HAZ (heat affected zone) when Charpy V-notch impact test were made at a low temperature ($1^{\circ}C$). Carbon steel plate (SA-516 Gr. 70) with thickness of 25mm for pressure vessel was welded by SMAW (shielded metal-arc welding) and specimens were fabricated from the welded plate. Charpy tests were then performed with specimens having different notch positions of specimens varying from the fusion line through HAZ to base metal. A series of finite element analysis which simulates the Charpy test and crack propagation initiating at the tip of V-notch was carried out as well. The finite element analysis takes into account the irregular fusion line and non-homogenous material properties due to the notch location of the specimen in HAZ. Results reveals that the energies absorbed during impact test depend significantly on the notch location and direction of specimen. Finite element analysis also demonstrates that the notch location of specimens, to a great extent, influences the reliability and consistency of the test.

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TiO2 성분 플럭스충진와이어에 따른 S500강의 GMA 용접부 특성 (Characteristics of GMA Weld Zone on TiO2 Different Component Flux Cored Wire for S500 Grade Steel)

  • 유철;고영봉;박경채
    • 한국표면공학회지
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    • 제48권6호
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    • pp.335-342
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    • 2015
  • Recently, the production of oil and gas at the arctic ocean and offshore has been growing. Accordingly, S500 steel with the high tensile strength and excellent toughness has been used and flux cored wire that can be welded to the S500 has been required. In this study, we carried out observation of microstructures, mechanical properties and CTOD (crack tip openning displacement) in the weld zone that GMA (gas metal arc) welded with different component of $TiO_2$ flux core wire (the main components, rutile or Ti-slag) for S500 steel. Weld zone produced with Ti-slag flux cored wire has formed a enough acicular ferrite and shown excellent impact toughness at $-40^{\circ}C$, tensile strength at room temperature and CTOD at $-20^{\circ}C$. As a result, the developed flux cored wire was suitable for S500 steel.

조선용 EH40 강판의 용접부 취성 균열전파정지에 관한 연구 (Study of Brittle Crack Propagation Welding for EH40 Steel Plate in Shipbuilding Steel)

  • 최경신;이상훈;정원지;황희건;홍석한;홍지웅
    • 한국기계가공학회지
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    • 제18권5호
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    • pp.9-16
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    • 2019
  • Recent economic trends are worsening and becoming longer, and Korean shipbuilding is focused on high value added and high technology, especially for LNG carriers and large container ships. Both ship types increased in size in the 2010s but have requirements such as high strength, toughness at low temperatures and continuous weldability for preventing brittle fractures at service temperatures. In particular, as container ships become larger, the International Classification Society (IACS) has established a provision (IACS UR S33) that mandates the use of BCA (Brittle Crack Arrest) certified vessels for large container vessels contracted after 2014 to ensure safety. Therefore, studies on BCA 47Y.P are currently being undertaken, but BCA 40Y.P has not been actively studied yet. We will test BCA 40Y.P to verify why it can be applied to a large container ship and measure fatigue cracking.

선박용 알루미늄 합금재의 부식피로균열 진전특성과 그 억제에 관한 연구 (Corrosion Fatigue Cracking Propagation Characteristics and its Protection for the AL-Alloys of Shipbuilding)

  • 임우조;김수병;이진열
    • 수산해양기술연구
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    • 제25권2호
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    • pp.87-104
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    • 1989
  • Recently, with the tendency of more lightening, high-strength and high-speed in the marine industries such as marine structures, ships and chemical plants, the use of the aluminium Alloy is rapidly enlarge and there occurs much interest in the study of corrosion fatigue crack characteristics. In this paper, the initiation of surface crack and the propagation characteristics on the base metal and weld zone of 5086-H116 Aluminium Alloy Plate which is one of the Al-Mg serious alloy(A5000serious) used most when building the special vessels, were investigated by the plane bending corrosion fatigue under the environments of marine, air and applying cathodic protection. The effects of various specific resistances on the initiation, propagation behavior of corrosion fatigue crack and corrosion fatigue life in the base metal and heat affected zone were examined and its corrosion sensitivity was quantitatively obtained. The effects of corrosion on the crack depth in relation to the uniform surface crack length were also investigated. Also, the structural, mechanical and electro-chemical characteristics of the metal at the weld zone were inspected to verify the reasons of crack propagation behavior in the corrosion fatigue fracture. In addition, the effect of cathodic protection in the fracture surface of weld zone was examined fractographically by Scanning Electron Microscope(S.E.M.). The main results obtained are as follows; (1) The initial corrosion fatigue crack sensitibity under specific resistance of 25Ω.cm% show 2.22 in the base metal and 19.6 in the HEZ, and the sensitivity decreases as specific resistance increases (2) By removing reinforcement of weldment, the initiation and propagation of corrosion crack in the HAZ are delayed, and corrosion fatigue life increases. (3) As specific resistance decreases, the sensitivity difference of corrosion fatigue life in the base metal and HAZ is more susceptible than that of intial corrosion fatigue crack. (4) Experimental constant, m(Paris' rule) in the marine environment is in the range of about 3.69 to 4.26, and as specific resistance increases, thje magnitude of experimental constant, also increases and the effect by corrosion decreases. (5) Comparing surface crack length with crack depth, the crack depth toward the thickness of specimen in air is more deeply propagated than that in corrosion environment. (6) The propagation particulars of corrosion fatigue crack for HAZ under initial stress intensity factor range of $\Delta$k sub(li) =27.2kgf.mm super(-3/2) and stress ratio of R=0 shows the retardative phenomenon of crack propagation by the plastic deformation at crack tip. (7) Number of stress cycles to corrosion fatigue crack initiation of the base metal and the welding heat affected zone are delayed by the cathodic protection under the natural sea water. The cathodic protection effect for corrosion fatigue crack initiation is eminent when the protection potential is -1100 mV(SCE). (8) When the protection potential E=-1100 mV(SCE), the corrosion fatigue crack propagation of welding heat affected zone is more rapid than that of the case without protection, because of the microfissure caused by welding heat cycle.

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20kHz 급 금속 초음파 융착용 스텝형 바 혼의 최적설계 (Analysis of Optimum Design of Stepped Bar Horn for 20kHz Metal Ultrasonic Welding)

  • 김지선;김재웅;김인주;서주환
    • 한국산학기술학회논문지
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    • 제20권12호
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    • pp.94-101
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    • 2019
  • 본 연구에서는 초음파 용접기의 진동에너지를 모재에 전달하는 금속 용접용 혼의 형상설계를 위해 해석적 기법을 적용하였으며, 20kHz 영역에서 사용되는 한파장 바 형상을 갖는 용접용 혼의 형상설계를 위해 FEM(Finite Element Method)을 사용하였다. 봉의 종진동 이론을 Ansys APDL(Ansys Parametric Design Language)에 적용하여 혼의 형상을 최적화하였다. 적절한 혼의 형상을 도출하기 위해 진동의 입력면과 출력면의 면적비와 혼의 축방향 길이비를 이용하여 총 25가지의 모델을 설계하였으며, Modal 해석과 Harmonic 해석을 통해 균일한 진동특성을 확보하고자 하였다. 스텝 바혼의 끝단부(팁)의 균일도 90%이상을 확보하기 위해 Harmonic 해석을 통해 길이비, 면적비를 결정하였고 이에 따라 혼의 총길이 130mm, 스텝 길이 65mm, 출력단 면적 28.79mm의 혼을 설계하였다. 설계치수를 바탕으로 Titanium (Ti-6Al-4V)-GR5 재료를 이용하여 혼을 제작하였다. 또한, 별도로 구성된 초음파 용접시스템을 이용하여 혼의 끝단부의 진동 진폭률 및 변위특성을 평가하였다. 최적화된 혼의 진폭률은 51%까지 향상됨을 확인하였다. 최종적으로 균일한 종방향 스텝 바혼을 설계하였으며, 끝단부(팁)의 균일도 97.4%이상을 확보하였다.

LNG 저장탱크 내조용 강 용접부의 파괴인성 평가 (Evaluation of Fracture Toughness in Steel Weldment for Inner Wall of LNG Storage Tank)

  • 장재일;주장복;양영철;김우식;홍성호;권동일
    • 한국가스학회지
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    • 제2권1호
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    • pp.7-13
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    • 1998
  • 본 연구에서는 LNG 저장탱크의 안전성을 확보하기 위한 연구의 일환으로서, 실제 탱크의 건설에서와 같은 조건으로 SMAW(Shielded Metal Arc Welding) 방식으로 용접된 $9\%$ Ni강의 X-개선 후판용접부내의 파괴인성의 변화를 평가하고 미세조직을 분석하였다. 이때 파괴인성의 평가는 본 연구자들이 제안한 '개선한 CTOD(crack tip opening displacement) 시험법'으로 행하였으며 열영향부내의 미세조직 및 파면은 광학현미경, 주사전자현미경 및 X-선 회절 분석기로 관찰하였다. 결과로부터 열영향부 내의 CTOD 값은, 평가위치가 용융선(Fusion Line-F.L.)으로 접근할수록 감소하는 경향을 나타내었다. 이는 잔류 오스테나이트의 양이 줄어들고 결정립 미세화 효과가 없어지는 영역인 결정립 조대화영역이 열영향 부내에서 차지하는 분율이 증가함에 따른 것이다. 한편, 잔류 오스테나이트의 열적 안정성이 상대적으로 감소하게 되는 F.L.${\~}$F.L.+3mm에서 온도감소에 따른 인성감소의 정도가 F.L.+5mm${\~}$F.L.+7mm보다 상대적으로 매우 큼을 알 수 있었다.

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용입부족을 가진 횡방향 맞대기 용접부의 피로특성에 관한 연구 (A Study on the Fatigue Characteristics in Butt-Welded Joints with Incomplete Penetration)

  • 장동일;경갑수;홍성욱
    • 한국강구조학회 논문집
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    • 제10권3호통권36호
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    • pp.497-508
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    • 1998
  • 본 연구에서는 평면결함의 일종인 용입부족의 크기가 맞대기 용접부의 피로 특성에 미치는 영향을 정량적으로 규명하였다. 정적실험 결과 비드를 삭제하지 않은 맞대기 용접부의 인장강도와 항복강도는 용입부족 크기에 관계없이 일정하였다. 또한 피로실험 결과 완전용입된 맞대기 용접부의 피로강도는 국내 외의 시방서에서 규정하고 있는 피로 등급을 모두 만족하며, 용입부족 크기에 따른 피로강도의 저하는 용입부족 크기가 증가함에 따라 피로강도가 급격하게 감소하였다. 파단형태에서 완전용입 시험체와 용입부족 시험체의 파단형태가 서로 다른 형식을 취하고 있음을 알 수 있었는데 이는 용접지단부와 용접루트부의 기하학적 형상에 따른 응력집중계수의 변화에 기인하는 것을 유한요소해석에서 확인하였다. 따라서 강구조물에 대한 용접제작시 발생할 수 있는 용접결함 중 평면결함의 일종인 용입부족은 반드시 피해야만 강구조물의 공용수명을 충분히 확보할 수 있을 것이다.

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MECHANICAL AND ADHESIONAL MANIPULATION TECHNIQUE FOR MICRO-ASSEMBLY UNDER SEM

  • Saito, Shigeki;Takahashi, Kunio;Onzawa, Tadao
    • 대한용접접합학회:학술대회논문집
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    • 대한용접접합학회 2002년도 Proceedings of the International Welding/Joining Conference-Korea
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    • pp.720-725
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    • 2002
  • In recent years, techniques for micro-assembly with high repeatability under a scanning electron microscope (SEM) are required to construct highly functional micro-devices. Adhesion phenomenon is more significant for smaller objects, becanse adhesional force is proportional to size of the objects while gravitational force is proportional to the third power of it. It is also known that adhesional force between micro-objects exposed to Electron Beam irradiation of SEM increases with the elapsed time. Therefore, mechanical manipulation techniques using a needle-shaped tool by adhesional force are often adopted in basic researches where micro-objects are studied. These techniques, however, have not yet achieved the desired repeatability because many of these could not have been supported theoretically. Some techniques even need the process of trial-and-error. Thus, in this paper, mechanical and adhesional micro-manipulation are analyzed theoretically by introducing new physical factors, such as adhesional force and rolling-resistance, into the kinematic system consisting of a sphere, a needle-shaped tool, and a substrate. Through this analysis, they are revealed that how the micro-sphere behavior depends on the given conditions, and that it is possible to cause the fracture of the desired contact interfaces selectively by controlling the force direction in which the tool-tip loads to the sphere. Based on the acquired knowledge, a mode diagram, which indicates the micro-sphere behavior for the given conditions, is designed. By refening to this mode diagram, the practical technique of the pick and place manipulation of a micro-sphere under an SEM by the selective interface fracture is proposed.

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Consideration of Methods Evaluating the Growing Process of Stress Corrosion Cracking of the Sensitized 18-8 Austenitic Stainless Steel in High Temperature Water Based on Electric Circuit Theory: The Effects of Stress Factors

  • Tsukaue, Yasoji
    • Corrosion Science and Technology
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    • 제6권3호
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    • pp.103-111
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    • 2007
  • The effect of stress factors on the growing process of stress corrosion cracking (SCC) of the sensitized 18-8 stainless steel in high temperature water was investigated using equations of crack growth rate derived from applying electric circuits to SCC corrosion paths. Three kinds of cross sections have to be considered when electric circuit is constructed using total current. The first is ion flow passage area, $S_{sol}$, of solution in crack, the second is total dissolving surface area, $S_{dis}$, of metal on electrode of crack tip and the third is dissolving cross section, $S_{met}$, of metal on grain boundary or in base metal or in welding metal. Stress may affect each area. $S_{sol}$ may depend on applied stress, $\sigma_{\infty}$, related with crack depth. $S_{dis}$ is expressed using a factor of $\varepsilon(K)$ and may depend on stress intensity factor, K only. SCC crack growth rate is ordinarily estimated using a variable of K only as stress factor. However it may be expected that SCC crack growth rate depends on both applied stress $\sigma_{\infty}$ and K or both crack depth and K from this consideration.$\varepsilon(K)$ is expressed as ${\varepsilon}(K)=h_2{\cdot}K^2+h_3{\cdot}K^3$ when $h_{2}$ and $h_{3}$ are coefficients. Also, relationships between SCC crack growth rate, da/dt and K were simulated and compared with the literature data of JBWR-VIP-04, NRC NUREG-0313 Rev.2 and SKIFS Draft. It was pointed out in CT test that the difference of distance between a point of application of force and the end of starter notch (starting point of fatigue crack) may be important to estimate SCC crack growth rate. An anode dissolution current density was quantitatively evaluated using a derived equation.