• Structural Engineering and Mechanics
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• 제75권5호
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• pp.559-569
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• 2020

In the present study, the fracture toughness of U-shaped notches made of aluminum alloy Al7075-T6 under combined tension/out-of-plane shear loading conditions (mixed mode I/III) is studied by theoretical and experimental methods. In the experimental part, U-notched test samples are loaded using a previously developed fixture under mixed mode I/III loading and their load-carrying capacity (LCC) is measured. Then, due to the presence of considerable plasticity in the notch vicinity at crack initiation instance, using the Equivalent Material Concept (EMC) and with the help of the point stress (PS) and mean stress (MS) brittle failure criteria, the LCC of the tested samples is predicted theoretically. The EMC equates a ductile material with a virtual brittle material in order to avoid performing elastic-plastic analysis. Because of the very good match between the EMC-PS and EMC-MS combined criteria with the experimental results, the use of the combination of the criteria with EMC is recommended for designing U-notched aluminum plates in engineering structures. Meanwhile, because of nearly the same accuracy of the two criteria and the simplicity of the PS criterion relations, the use of EMC-PS failure model in design of notched Al7075-T6 components is superior to the EMC-MS criterion.

• 한국항공우주학회지
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• 제31권7호
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• pp.63-68
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• 2003

쇼트피닝 가공은 금속부품의 피로특성 향상을 위해 대부분 널리 이용되고 있는 방법이다. 쇼트피닝 가공에 있어 재현성이 있고 신뢰할 수 있는 최적화된 피로특성 증가를 위해 가장 중요한 점이 쇼트피닝 변수 조절이다. 본 논문에서는 최적 피닝강도(알멘강도) 조건에 대한 실험적인 연구가 수행되었다. 피로 특성에 관한 최적피닝의 효과를 검토하기 위하여 회전굽힘피로시험법을 채택하였다. 실험 결과 피로강도와 피로수명이 최적피닝 조건에 의해 크게 증가하였으나 언더피닝 및 오버피닝의 경우에는 감소함을 보였다.

• 대한기계학회논문집A
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• 제35권10호
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• pp.1347-1353
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• 2011

마찰교반용접은 일반적인 용접법에 비하여 기계적 성질, 용접결함의 감소, 재료 절감 그리고 짧은 생산시간과 같은 장점 때문에 제작공정에 광범위하게 사용되고 있다. 본 연구의 목적은 이전의 실험 결과를 이용하여 마찰교반용접의 최적 조건을 검토하고 최적의 마찰용접조건에서 접합된 7075-T651 알루미늄 판재의 3가지 다른 영역, 즉 용접재, 열영향부재 그리고 모재에 대한 피로균열전파의 거동을 고찰하는 것이다. 최적의 마찰교반용접조건은 회전속도 800rpm, 이송속도 0.5mm/sec로 결정되었으며, 최적의 마찰교반용접에서 용접된 시험편에 대한 피로균열전파율은 3가지 영역의 재질, 즉 용접재, 열영향부재, 모재와 균열의 구동력에 크게 의존함을 보였다.

• 열처리공학회지
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• 제11권3호
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• pp.200-206
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• 1998

The aim of this study is to investigate the effect of impurity level and fabrication processes on the strength, impact and fracture toughness of 7075, 7050 and 7175 aluminum alloy forgings. A specially processed 7175S-T74 aluminum forgings was superior to a conventionally processed 7075-T73, 7050-T74 and 7175-T74 aluminum forgings in both strength and toughness. The reduction of impurity level of iron and silicon has significantly diminished the size and volume fraction of second phase particles such as $Al_7Cu_2Fe$ and $Mg_2Si$. A further reduction of the amount of second phase particles has been observed by applying a special fabrication process. This phenomena result from the application of intermediate soaking at higher temperature and more sufficiant hot working temperature than that of a conventional processing.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 1995년도 제5회 학술강연회논문집
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• pp.195-203
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• 1995

본 연구는 강도와 인성이 우수한 7175Al 단조재의 국산화 개발을 위하여 기존 7XXX합금의 제조공정(일반공정)을 적용한 7075-T6/T73, 7050-774 및 7175-T74 단조재와 중간열처리, 용체화처리 등을 고온처리하는 특수제조 공정을 적용한 7175-T74 단조재의 강도, 파괴인성($K_IC$) 및 피로특성을 비교 평가하였다. 특수공정을 적용한 7175S-T74 단조재는 일반공정의 7075-T73, 7050-T74 및 7175-T74재보다 강도, 파괴 인성 및 피로특성이 향상되었다. 이것은 주조시 응고과정에서 형성되는 2차상입자의 감소와 특수공정의 적용효과에 기인하는 것으로 판단된다.

• 한국세라믹학회지
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• 제34권5호
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• pp.483-490
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• 1997

Al2O3/metal composites were fabricated by oxidation and reaction of molten Al-alloy into two types of commercial Al2O3-SiO2 fibrous insulation board. The growth rate, composition and microstructure of these materials were described. An AlZnMg(7075) alloy was selected as a parent alloy. Mixed polycrystalline fiber and glass phase fiber were used as a filler. The growth surface of an alloy was covered with and without SiO2. SiO2 powder was employed as a surface dopant to aid initial oxidation of Al-alloy. Al-alloy, SiO2, fiber block and growth inhibitor CaSiO3 were packed sequentially in a alumina crucible and oxidized in air at temperature range 90$0^{\circ}C$ to 120$0^{\circ}C$. The growth rate of composite layer was calculated by measuring the mass increasement(g) per unit surface($\textrm{cm}^2$). XRD and optical microscope were used to investigate the composition and phase of composites. The composite grown at 120$0^{\circ}C$ and with SiO2 dopant showed rapid growth rate. The growth behavior differed a little depending on the types of fiber used. The composites consist of $\alpha$-Al2O3, Al, Si and pore. The composite grown at 100$0^{\circ}C$ exhibited better microstructure compared to that grown at 120$0^{\circ}C$.

• 한국재료학회지
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• 제6권10호
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• pp.1043.1-1048
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• 1996

알루미나 매트릭스 복합재료를 AIZnMg(7075)-합금의 직접적인 용융산화를 통하여 제조하였다. 충전재료는 17$\mu\textrm{m}$ 크기의 모서리가 둥근 연마재용 SiC 입자를 사용하였다. 산화촉진재 SiO2를 사용한 경우와 사용하지 않은 경우를 비교하였다. 매트릭스 형성 매카니즘과 반응거동을 온도와 SiO2사용량을 중심으로 연구하였으며, 얻어진 AI2O3/SiC/금속 복합재료의 미세구조를 관찰하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회A
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• pp.274-278
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• 2007

The purpose of this study is to analyze the important loads related with crack-growth in aircraft. Al Alloys mainly used in aircraft are Al2024 and Al7075 in Duralumin. In random fatigue loading, it has been understood crack-growth characteristic using fractured surface photograph by SEM. In order to obtained CTOD, we measured a crack size in wing frame part. As a result of fatigue experiment that accumulating plenty of fatigue loadings, we find more cracks than that produces in the same fatigue loading. The important loads relating to crack-growth was found in the largest strain cycle. Applying strain block in fatigue experiment, it is actually loading in connection of aircraft. In conclusion, These results can be used for preventing an accident owing fatigue-fracture in aircraft.

• 대한기계학회논문집
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• 제17권7호
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• pp.1751-1760
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• 1993

The squeeze casting process is considered as an attractive way to form the primary product of near net shape metal matrix composites for wide use in automobile industry. To understand for infiltration limit in squeeze casting processes, the SAFFIL short fiber preform of volume fraction $10%{\sim}23%$ were fabricated by vaccum pumping and speed control press, and the optimal condition for fiber preform fabrication had been experimentally obtained. The composite materials were fabricated by forced infiltration of molten metals such as Al6061, Al7075, pure Al, AC8A, and Al2024. The infiltration distance and deformation of fiber preform are observed, and tensile strength were measured from at the room temperature.

• 한국분말야금학회:학술대회논문집
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• 한국분말야금학회 2006년도 Extended Abstracts of 2006 POWDER METALLURGY World Congress Part 1
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• pp.536-537
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• 2006

In the present work, the sintering behavior of high strength Al-5.6Zn-2.5Mg-1.6Cu (in wt.%) alloy compacts prepared from elemental powders was investigated. Microstructural evaluation was accompanied by XRD and DSC methods in order to determine the temperature and chemical composition of the liquid phases formed during sintering. It was found that three transient liquid phases are formed at 420, 439 and 450 $^{\circ}C$. Microstructural study revealed the progressive formation of sintered contacts due to the presence of the liquid phases, although the green compact expands as a result of the melt penetration along the grain boundaries. While Zn melts at ${\sim}420\;^{\circ}C$, the intermetallic phases formed between Al and Mg were found to be responsible for the formation of liquid phase and the dimensional change at higher temperatures.