• 제목/요약/키워드: 2xxx series aluminum alloy

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Effect of Compacting Pressure on Sintering Characteristics of Commercial 2xxx Series Al Alloy Powders (성형압의 변화가 상용 2xxx AI 합금계 혼합분말의 소결특성에 미치는 영향)

  • 김대건;민경호;장시영;김영도
    • Journal of Powder Materials
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    • v.9 no.2
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    • pp.116-123
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    • 2002
  • The characteristics of two commercial 2xxx series Al alloy powders, AMB2712 and 201AB, were evaluated and their compacting and sintering characteristics were discussed in tems of compacting pressure. The particle shapes of both two powder mixtures were irregular and their particle size distributions were broad. The compactibility of AMB2712 was superior to that of 201AB because of better fluidity. The sintered density was higher than the green density at low compacting pressure, however, it was lower than the green density when the samples were compacted at higher pressure due to the selling during sintering. The sintered density was alomost the same as the green density at the "homogeneous deformation" stage. It was observed that pores were created at the triple points due to the rapid diffusion of Cu in Al. Cu in Al.

Stress Corrosion Cracking Sensitivity of High-Strength 2xxx Series Aluminum Alloys in 3.5 % NaCl Solution (항공용 고강도 2xxx계 알루미늄 합금의 3.5 % 염수 환경에서의 응력부식균열 민감도)

  • Choi, Heesoo;Lee, Daeun;Ahn, Soojin;Lee, Cheoljoo;Kim, Sangshik
    • Korean Journal of Materials Research
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    • v.28 no.12
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    • pp.738-747
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    • 2018
  • For the aerospace structural application of high-strength 2xxx series aluminum alloys, stress corrosion cracking(SCC) behavior in aggressive environments needs to be well understood. In this study, the SCC sensitivities of 2024-T62, 2124-T851 and 2050-T84 alloys in a 3.5 % NaCl solution are measured using a constant load testing method without polarization and a slow strain rate test(SSRT) method at a strain rate of 10-6 /sec under a cathodic applied potential. When the specimens are exposed to a 3.5 % NaCl solution under a constant load for 10 days, the decrease in tensile ductility is negligible for 2124-T851 and 2050-T84 specimens, proving that T8 heat treatment is beneficial in improving the SCC resistance of 2xxx series aluminum alloys. The specimens are also susceptible to SCC in a hydrogen-generating environment at a slow strain rate of $10^{-6}/sec$ in a 3.5 % NaCl solution under a cathodic applied potential. Regardless of the test method, low impurity 2124-T851 and high Cu/Mg ratio 2050-T84 alloys are found to have relatively lower SCC sensitivity than 2024-T62. The SCC behavior of 2xxx series aluminum alloys in the 3.5 % NaCl solution is discussed based on fractographic and micrographic observations.

Stress Corrosion Cracking of High Strength Al-Zn-Mg-Cu Aluminum Alloy with Different Compositions (고강도 Al-Zn-Mg-Cu 합금에서 조성에 따른 응력부식균열 특성)

  • Kim, Jun-Tak;Kim, Sang-Ho
    • Journal of the Korean institute of surface engineering
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    • v.41 no.3
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    • pp.109-113
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    • 2008
  • High strength 7xxx series Al-Zn-Mg alloy have been investigated for using light weight automotive parts especially for bump back beam. The composition of commercial 7xxx aluminum has the Zn/Mg ratio about 3 and Cu over 2 wt%, but this composition isn't adequate for appling to automotive bump back beam due to its high resistance to extrusion and bad weldability. In this study the Zn/Mg ratio was increased for better extrusion and Cu content was reduced for better welding. With this new composition we investigated the effect of composition on the resistivity against stress corrosion cracking. As the Zn/Mg ratio is increased fracture energy obtained by slow strain rate test was decreased, which means degradation of SCC resistance. While the fracture energy was increased with Cu contents although it is below 1%, which means improvement of SCC resistance. These effects of composition change on the SCC resistivity were identified by observing the fracture surface and crack propagation.

Improvement of Fracture Toughness in 7XXX Series Aluminum Alloy Forings (7XXX계 알루미늄합금 단조재의 파괴인성 개선)

  • Song, K.H.;Lee, O.H.
    • Journal of the Korean Society for Heat Treatment
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    • v.11 no.3
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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.

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A Study on Derivation of Contact Heat Transfer Coefficient Between Die and Aluminum Billet in High Temperature Compression Process (고온 압축 공정에서 금형과 알루미늄 빌렛의 접촉 열전달 계수 도출에 관한 연구)

  • Jeon, H.W.;Suh, C.H.;Oh, S.G.;Kwon, T.H.;Kang, G.P.;Yook, H.S.
    • Transactions of Materials Processing
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    • v.30 no.3
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    • pp.142-148
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    • 2021
  • In hot forging analysis, the interfacial heat transfer coefficient (IHTC) is a very important factor defining the heat flow between the die and the material. In particular, in the hot forging analysis of aluminum 6xxx series alloy, which are used in automobile parts, differences in load and microstructure occur due to changes in surface temperature according to the IHTC. This IHTC is not a constant value but changes depends on pressure. This study derived the IHTC under low load using aluminum 6082 alloy. An experiment was performed by fabricating a compression die, and a heat transfer analysis was performed based on the experimental data. The heat transfer analysis used DEFORM-2D, a commercial finite element analysis program. To derive the IHTC, heat transfer analysis was performed for the IHTC in the range of 10 to 50 kW/m2℃ at intervals of 10kW/m2℃. The heat transfer analysis results according to the IHTC and the actual experimental values were compared to derive the IHTC of the aluminum 6082 alloy under low load.

Analysis of Weld Characteristics for Aluminum 5XXX Series Laser Welding Using 3-Dimension Remote Scanner (3차원 원격 스캐너를 이용한 알루미늄 5000 계열의 레이저 용접에서 공정 변수에 따른 용접 특성 분석)

  • Kim, D.Y.;Park, Y.W.
    • Laser Solutions
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    • v.14 no.2
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    • pp.1-7
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    • 2011
  • The latest trends of vehicle technology development are fuel efficiency improvement, body designs declining air resistance and lightweight of materials. Especially, as lightened weight of materials makes engine efficient so that vehicles keep the best performance, it is the best way to protect the environment and reduce fuel consumption. In this study, we conducted laser welding by using 3-dimension remote scanner that is 5J32 aluminium alloy. Furthermore, conduction experiment that was 3 times repeated for changing factors such as observing angle, laser power and welding speed. we observed exterior and cross section of weled part and tensile strength. When increasing laser power and decreasing laser speed, tensile strength increased. In order to evaluate factors that affect tensile strength qualitatively we conducted ANOVA. We assumed that the factors are observing angle, laser power and welding speed. Then we found that laser power and laser speed affect tensile strength. We conducted evaluation of weldability of aluminium alloy by above ways.

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Effect of Fabrication Processes on the Fatigue and Fracture Toughness of 7XXX Series Aluminum Forgings (7XXX계 단조재의 피로 및 파괴인성에 미치는 제조공정의 영향)

  • Lee, O.H.;Lim, J.K.;Song, K.H.;Son, Y.I.;Eun, I.S.;Shin, D.S.
    • Journal of the Korean Society for Heat Treatment
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    • v.9 no.3
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    • pp.161-168
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    • 1996
  • The purpose of this study is to investigate the effect of impurity level and fabrication processes on the strength, fracture toughness and fatigue resistance of 7075, 7050 and 7175 high strength aluminum forgings. It has been verified that plane strain fracture toughness and fatigue characteristics of a specially processed 7175S-T74 alloy is superior to a conventionally processed 7075-T6/T73, 7050-T74 and 7175-T74 alloys. These beneficial effects primarily arise from two view points, i.e., the effect of reducing the impurity level of iron and silicon has significantly diminished the size and volume fraction of second phase particles such as $Al_7Cu_2Fe$ and $Mg_2Si$. Futher reduction of the amount of nonequilibrium second phase particles has been observed by applying a special fabrication process.

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