• Journal of Welding and Joining
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• 제12권1호
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• pp.38-43
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• 1994

고강도 알루미늄합금은 중량이 가벼우면서 인장강도와 항복강도가 높고 가공성, 성형성이 좋아 항공기, 자동차, 선박 등 수송용 재료로 각광을 받고 있으며, 이 중 Al-Zn-Mg계(7000계) 알루미늄 합금은 용접 구조물용 경량소재로 활용범위가 높다. Al-Zn-Mg계 알루미늄 합금은 고온에서 용체화 처리후 저온으로 급냉시킨 재료를 자연시효 또는 인공시효처리를 하여 이 때 석출되는 시효 석출물에 의해 강도를 증가시킨 석출 경화형 합금이다. 그런데, 7000계열 알루미늄합금은 적절한 열처리 작업을 통해 최적의 기계적 성질이 얻어지도록 합금설계가 되어있기 때문에 구조물 제작시 용접에 의한 ARC 열을 받게 되면 열이력(thermal cycle)에 의해 모재의 미세조직이 변화하고 용접 결함이 발생하며 강도의 약화와 함께 내식성 등이 저하한다. 따라서 고강도 알루미늄합금의 용접성을 향상시키기 위해서는 용접부의 미세조직거동과 용접부에 발생하는 용접결함의 현상을 조사하여 용접용 고강도 합금에 필수적으로 요구되는 용접성에 대한 검토가 충분히 이루어져야 한다. 따라서 본 고에서는 알루미늄합금, 특히 7000계열 알루미늄합금에 주목하여, 용접방법, 각종 결함과 대책, 용접부의 시효경화와 응력부식균열 및 기계적 성질 등을 지금까지 보고된 각종 자료를 기초로 하여 3회에 걸쳐 기술하고자 한다.

• 대한용접접합학회:학술대회논문집
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• 대한용접접합학회 2005년도 춘계학술발표대회 개요집
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• pp.226-228
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• 2005

Of typical welding techniques, to employ the heat for joining process is the most commonly used welding process. But there arise difficulties when this process is applied to light weight alloys such as Aluminium alloy. In this respect, Friction Stir Welding(FSW), a solid-state joining process, is the most effective welding technique with significant potential for various industrial applications. In this study, the characteristics of lapping FSW Al 5052 alloy are shown under a variety of welding parameters such as the rotation speed of FSW tool and welding velocity. Conclusively, the welding properties of lapping FSW Al 5052 were found to be dominated by the deformation of non-joining area near the welding nugget rather than other factors such as the thermal input.

• Journal of Advanced Marine Engineering and Technology
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• 제23권4호
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• pp.523-532
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• 1999

This study is aimed to obtain fundamental knowledge of pulse laser welding phenomena the authors investigated the structure and composition of evaporated particles of Al alloys in air and in the Ar atmosphere during pulsed laser welding. The ultra-fine particles of 5 to 100nm diameter in a globular or irregular shape were formed in laser-induced plasma and the main structure was $MgAl_2O_4$ The composition of particles was ifferent depending on the power density of a laser beam; namely under the low power density conditions magnesium was predominant in the parti-cles while aluminium content increased with an increase in the power density. These results were attributed to evaporation phenomena of metals with different boiling points and latent heats of vaporization. On the other hand the number density of laser-induced plasma species was obtained by Saha's equation. it was confirmed that the number density depends upon the plasma tempera-ture and total pressures.

• 한국해양공학회지
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• 제15권2호
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• pp.94-98
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• 2001

fatigue life and nondestructive evaluation were examined experimentally using surface crack specimen and compact tension specimen of 5083 aluminium alloy. Acoustic emission signals emanated during failure of aluminum alloys has been the subject of numerous investigations. Possible sources of AE during deformation have been suggested as the dislocations, fracture of brittle particles and debonding of these particles from the alloy matrix. Fatigue life and penetration behavior of long surface crack can be evaluated quantitatively using K values proposed by authors. The influence of stress ratio on the frequency characteristics of AE signals were investigated.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2003년도 추계학술대회 논문집(III)
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• pp.49-58
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• 2003

In this paper, the structural strengths of a rolling stock seat were numerically evaluated under several design load conditions based on the UIC requirements. The rolling stock seat was designed for the high speed train of a Chinese conventional line. To maximize its weight reduction and structural strength, some aluminium alloys like 6N01-T5 and ALDC8-T5 were applied to the base frame, side frame and armrest. The designed seat frame satisfied the strength requirements on inertia loads due to accelerations, and fatigue test conditions. However, it violated the requirements on the static test of UIC 566 OR. Some design modifications were suggested and numerically evaluated to satisfy the static test requirements.

• 한국표면공학회지
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• 제53권1호
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• pp.36-42
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• 2020

In this study, two novel methods to measure the surface hardness of anodic oxide films on aluminum alloys are reported. The first method is to impregnate oil-based ink into pores in the anodic oxide film and then to clean the ink on the surface using ethanol, resulting in an impregnation of inks only inside of the pores in anodic oxide film. The second method is to coat the anodic oxide film surface with thin Au layer less than 0.1 ?. Both the ink-impregnating method and Au-coating method provided clear indentation marks on the anodic oxide film surface when it was indented using a pyramidal-diamond penetrator. Thus, Vickers hardness of anodic oxide films on aluminium alloy could be measured successfully and precisely from the anodic film surface. In addition, advantages and disadvantages of the ink-impregnating method and Au-coating method for the measurement of surface hardness of anodic oxide films are discussed.

• 한국항해항만학회지
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• 제31권10호
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• pp.825-831
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• 2007

일반적으로 선박 및 해양구조물에서 사용하고 있는 고강도 알루미늄 재료들은 일반 강재에 비해서 많은 이점들을 가지고 있다. 이러한 알루미늄 재료들은 여러 분야에 걸쳐서 폭넓게 사용되고 있으며, 특히, 초고속 선박의 선체와 갑판부에 많이 이용되어지고 있고, 교량구조물에 사용되는 박스 거더, 그리고 해양구조물의 갑판부와 선측구조에도 널리 이용되고 있다. 이러한 알루미늄 구조는 전체적인 구조부재의 중량을 감소하게 하면서 선속의 증가를 가져온다. 일반적인 강구조물의 응력-변형률 관계와 비교하여 보면, 용접가공에 의하여 발생되는 열영향부의 존재로 인하여 상당히 다르게 나타난다. 왜냐하면, 강구조물에 비해 열전도율이 높아서, 열영향부(heat affected zone, HAZ)의 영향이 크게 작용하기 때문이다. 본 논문에서는 종방향 압축하중을 받는 알루미늄 보강 판넬의 최종강도 특성에 대하여, 열영향부의 범위를 변화한 유한요소해석을 통하여, 열영향부의 범위와 파굴 및 최종강도 거동의 관계에 대해서 고찰하였다.

• 해양환경안전학회지
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• 제20권6호
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• pp.738-745
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• 2014

본 논문에서는 탄소성 영역 내 패치 로딩 크기에 따른 알루미늄 합금 사각형 판의 초기 처짐 영향을 수치해석방법으로 이용한 탄성 및 탄소성 대변형 시리즈 해석을 수행하였다. 주변 지지조건은 단순지지로 가정하고 초기 처짐 크기(w/t), 종횡비(a/b), 세장비(b/t)를 고려하여 알루미늄 합금 A6082-T6 사각형 판의 임계 탄성 좌굴하중과 좌굴 후 거동을 검토하였다. 탄성 및 탄소성 대변형 시리즈 해석은 상용프로그램을 사용하였다. 초기 처짐 크기가 작을 경우 하중증가와 함께 면내 강성이 처음부터 감소하며 크기가 커질수록 훨씬 두드러지게 발생한다. 종횡비가 커질수록 초기항복강도는 점차 감소하며 판 두께가 두꺼울수록 패치 로딩 크기(l/b) 0.5 이후 초기 항복강도 감소비율은 얇은 두께보다 더 크게 발생한다.

• 한국분말재료학회지
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• 제9권6호
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• pp.441-448
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• 2002

Dispersions of non-soluble ceramic particles in a metallic matrix can enhance the strength and heat resistance of materials. With the advent of mechanical alloying it became possible to put the theoretical concept into practice by incorporating very fine particles in a flirty uniform distribution into often oxidation- and corrosion- resistant metal matrices. e.g. superalloys. The present paper will give an overview about the mechanical alloying technique as a dry, high energy ball milling process for producing composite metal powders with a fine controlled microstructure. The common way is milling of a mixture of metallic and nonmetallic powders (e.g. oxides. carbides, nitrides, borides) in a high energy ball mill. The heavy mechanical deformation during milling causes also fracture of the ceramic particles to be distributed homogeneously by further milling. The mechanisms of the process are described. To obtain a homogeneous distribution of nano-sized dispersoids in a more ductile matrix (e.g. aluminium-or copper based alloys) a reaction milling is suitable. Dispersoid can be formed in a solid state reaction by introducing materials that react with the matrix either during milling or during a subsequent heat treatment. The pre-conditions for obtaining high quality materials, which require a homogeneous distribution of small dis-persoids, are: milling behaviour of the ductile phase (Al, Cu) will be improved by the additives (e.g. graphite), homogeneous introduction of the additives into the granules is possible and the additive reacts with the matrix or an alloying element to form hard particles that are inert with respect to the matrix also at elevated temperatures. The mechanism of the in-situ formation of dispersoids is described using copper-based alloys as an example. A comparison between the in-situ formation of dispersoids (TiC) in the copper matrix and the milling of Cu-TiC mixtures is given with respect to the microstructure and properties, obtained.

• 한국금형공학회:학술대회논문집
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• 한국금형공학회 2008년도 하계 학술대회
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• pp.39-44
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• 2008

Magnesium alloys have given high attention to the industry of light-weigh as automobile and electronics with aluminium, titanium and composite alloys due to their high strength, low specific density and good damping characteristics. But the magnesium contained structures under high temperature have the problems related to creep deformation and rupture life, which is a reason of developing the new material against creep deformation to use them safely. The purpose of this study is to predict the creep deformation mechanism and rupture time of AZ31 magnesium alloy. For this, creep tests of AZ31 magnesium alloy were done under constant creep load and temperature with the equipment including automatic temperature controller with acquisition computer. The apparent activation energy Qc and the applied stress exponent n, rupture life have been determined during creep of AZ31 Mg alloy over the temperature range of $150^{\circ}C$ to $300^{\circ}C$. In order to investigate the creep behavior. Constant load creep tests were carried out in the equipment including automatic temperature controller, whose data are sent to computer. At around the temperature of $150^{\circ}C{\sim}300^{\circ}C$ the creep behavior obeyed a simple power-law relating steady state creep rate to applied stress and the activation energy for the creep deformation was nearly equal and a little low, respectively, to that of the self diffusion of Mg alloy.