• Title/Summary/Keyword: Al7050 합금

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The Surface Modification and Low Cycle Fatigue Behavior of N+ion Implantated 7050Al Alloy (질소 이온 주입시킨 7050Al합금의 표면 미세구조 변화와 저주기 피로거동)

  • Lee, C.W.;Kwun, S.I.
    • Journal of the Korean Society for Heat Treatment
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    • v.7 no.4
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    • pp.307-317
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    • 1994
  • The surf ace microstructure modification by $N^+$ ion implantation into 7050Al alloy and its low cycle fatigue behavior were investigated. Ion implantation method is to physically implant accelerated ions to the surface of a substrate. High dose of nitrogen($5{\times}10^{17}ions/cm^2$) were implanted into 7050Al alloy using current density of accellerating voltage of 100KeV. The implanted layers were characterized by Electron Probe-Micro Analysis(EPMA), Auger Elecron Spectroscopy(AES), X-Ray Diffraction(XRD), X-Ray Photoelectron Spectroscopy(XPS), and Transmission Electron Microscopy(TEM). The experimental results were compared with computer simulation data. It was shown that AlN was formed to 4500 ${\AA}$ deep. The low cycle fatigue life of the $N^4$ion modified material was prolonged by about three times the unimplanted one. The improved low cycle fatigue life was attributed to the formation of AlN and the damaged region on the surface by $N^+$ ion implantation.

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Correlation Between Tensile-compressive Behavior and Formability of Al7050 Alloy (Al7050 합금의 인장-압축거동과 성형성 간 상관관계)

  • Bae, D.H.;Oh, J.H.;Jeong, C.;Kim, J.G.
    • Transactions of Materials Processing
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    • v.31 no.2
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    • pp.64-72
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    • 2022
  • Since aluminum alloys experience both tensile and compression deformation modes during forming process, it is important to understand the role of deformation mode on the hot formability of metallic alloys. In the present work, the hot formability of Al7050 alloy was investigated by conducting both tensile and Gleeble tests at various temperatures and strain rates. Processing maps representing low efficiency regions were observed at low temperature and high strain rate in both tensile and compressive deformation modes while the maximum efficiency regions depended on different deformation modes. Moreover, samples tested at stable processing conditions presented a smaller pore fraction than those at instable conditions that resulted in crack initiation during plastic deformation. This result shows that different deformation modes during plastic forming can affect formability changes of metallic alloys. Understanding of tension-compression behaviors will help us solve this problem.

The Effect of Thermomechanical Treatment on the Microstructural Changes and Fatigue Properties in 7050 Al Alloy (7050 AI 합금의 가공열처리가 미세조직변화와 피로성질에 미치는 영향)

  • Kim, M.H.;Kwun, S.I.
    • Journal of the Korean Society for Heat Treatment
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    • v.4 no.4
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    • pp.24-33
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    • 1991
  • The effects of thermomechanical treatments on microstructure and fatigue properties of 7050 Al alloy were investigated. The precipitation kinetics changed to a faster rate due to cold deformation employed in this special TAHA thermomechanical treatments including pre-aging, plastic deformation and two step final-aging. The G.P. zones in the under-aged condition were cut by dislocations and dissolved during the plastic deformation. During the low cycle fatigue, the T6' condition showed cyclic hardening behavior whereas the TMT5, TMT27 and T76 conditions showed cyclic softening at above 0.7% total strain amplitudes. The ${\Delta}K_{th}$ value of TMT27 was improved more than two times, compared with that of T76 condition. The T6' with small shearable precipitates resulted in the markedly high ${\Delta}K_{th}$ value. This is thought to be resulted from dislocation reversibility and roughness-induced crack closure due to planarity of slip.

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A Study on Fretting Fatigue of High Strength Aluminum Alloys (고강도 알루미늄 합금의 Fretting Fatigue에 관한 연구)

  • Lee, Hak-Sun;Kim, Sang-Tae;Choi, Sung-Jong;Yang, Hyun-Tae;Kim, Jae-Kyoung;Lee, Dong-Suk
    • Proceedings of the KSME Conference
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    • 2004.04a
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    • pp.168-173
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    • 2004
  • Fretting is a kind of surface degradation mechanism observed in mechanical components and structures. The fretting damage decrease in 50-70% of the plain fatigue strength. This may be observed in aircraft, automobile and nuclear power plant used in special environment and various loading conditions. In the present study, the characteristics of the fretting fatigue are investigated using the two aluminum alloy(Al2024-T3511 and Al7050-T7451). Through the experiment, it is found that the fretting fatigue strength of the Al7050-T7451 alloy decreased about 50% from the plain fatigue strength, while the fretting fatigue strength of the Al2024-T3511 alloy decreased about 45%. The tire track was widely observed in fracture surface area of oblique crack which was induced by contact pressure. These results can be the basic data to the structural integrity evaluation of aluminum alloy subjected to fretting damage.

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A Study on the RRA(Retrogression and Reaging) treatment of 7050 Al alloy (7050 Al 합금의 RRA 처리에 관한 연구)

  • Choi, Joong-Whoan;Kim, Jang-Ryang;Lee, Sang-Lae;Kim, In-Bae
    • Korean Journal of Materials Research
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    • v.10 no.7
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    • pp.493-498
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    • 2000
  • The effects of RRA treatment on the microstructures and mechanical properties of 7050 Al alloy were investigated by differential scanning calolimetry, transmission electron microscopy, microhardness measurement and electrical conductivity. The hardness of 2nd-step aged specimen at $175^{\circ}C$ was decreased to mimimum value and increased to a peak hardness, and then re-decreased with retrogression treatment. It was found that the hardness of 2nd-step aged specimen was further increased by 3rd step aging treatment($120^{\circ}C$x24h). The initial decrease in hardness during 2nd-step aging was due to the partial dissolution of pre-existing GP zone, the major precipitation hardening phase at T6 condition. It was confirmed that the major precipitation hardening phase at 3rd-step aging was GP zone and η' phase. The electrical conductivity increased continually through 2nd-step and 3rd-step aging treatment. It was conclude that the optium 2nd-step aging condition was at $175^{\circ}C$ for 50min by considering the hardness and electrical conductivity.

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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 the Forging Prototype Manufacture of Aluminium 7050 Alloys (Al7050합금의 단조 시제품 제작에 관한 연구)

  • Kang, Seong-Ki;Lee, Jea-Kun
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.11 no.4
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    • pp.39-45
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    • 2012
  • In this paper, process conditions are investigated for elimination of the grain coarsening and improved material flow during forging process by both of experiments and FEM analysis. Particular interest has been given to understand role of preform shape on the grain coarsening behavior and magnitude of the hammer forging load. As the results of FEM simulation by using DEFORM-3D, the simulated forging loads were 2,200ton in the case of a machined bar which is machined from 65mm to 60mm diameter, and below 1,900ton in the case of machined preform, respectively. The use of preform has been beneficial for reduction of the forging load and elimination of the grain coarsening. However, in the case of as received bar and the round bar, which was machined to 2.5mm thickness in surface layer, some degree of local grain coarsening behavior has been observed. The optimized preform shape could be properly designed by applying the FEM simulation.

7XXX계 단조재의 피로 및 파괴인성 개선

  • 황성주;임재규;이오연;손영일;은일상;신돈수
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1995.11a
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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.

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A Syudy on the Diffusion Joining of 7000 Al Alloy (7000계 Al 합금의 확산접합에 관한 연구)

  • Jin, Y.C.;Hong, E.S.;Kim, Y.S.;Lee, M.S.;Yoo, C.Y.
    • Journal of the Korean Society for Heat Treatment
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    • v.6 no.1
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    • pp.9-16
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    • 1993
  • To investigate the properties of diffusion bonding of 7050 Al alloy, the diffusion bonding joints have been produced in self-made diffusion bonding hot-press which admits a defined application of the bonding pressure during the heating phase and also rapid cooling after the bonding process with various bonding condition. The strength of the bond increases with increasing the bonding time and temperature. Shear test at toom temperature showed that high strength up to 70% that of parent metal (320 MPa), 220 MPa for the specimen bonded 14 hr at $560^{\circ}C$, with 3 MPa. In this case, however, there is large deformation more than 20% reduction in thickness. The results were correlated with joint characteristics found by optical microstructure and by fractography by SEM. When the strengths of the bonds are more than 50% that of parent metal, a great deal of dimples stretched along the direction of shear stress are observed over the fractured surface of the bond. On the microstructure of the bond line, initial mophology of the bond line disapeared for the grain boundary migration with increasing the bonding time.

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TEM Analysis on Oxide Films of Al1050 and Al7075 Exposed to 24-month Atmospheric Conditions (24개월 대기 노출된 Al1050 및 Al7075 알루미늄 합금 산화막에 대한 투과전자현미경 분석)

  • Kim, Dae-Geon;Kim, Ga-Rim;Choi, Wonjun;Bahn, Chi Bum
    • Journal of the Korean institute of surface engineering
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    • v.52 no.2
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    • pp.62-71
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    • 2019
  • Al1050 and Al7075 alloy specimens were exposed to atmospheric conditions for 24 months and analyzed by Transmission Electron Microscopy to characterize their corrosion behavior and oxide film characteristics, especially focusing on intergranular corrosion or oxidation. In general, the intergranular oxygen penetration depth of Al1050 was deeper than Al7075. Since O and Si signals were overlapped at the oxidized grain boundaries of Al1050 and Mg is not included in Al1050, it is concluded that Si segregated along the grain boundaries directly impacts on the intergranular corrosion of Al1050. Cr-Si or Mg-Si intermetallic particles were not observed along the grain boundaries of Al7050, but Mg-Si particle was barely observed in the matrix. 10-nm size Mg-Zn particles were also found all over the matrix. Mg was mainly observed along the oxidized grain boundary of Al7075, but Si was not detected due to the Mg-Si particle formation in the matrix and relatively low concentration of Si in Al7075. Therefore, it is thought that Mg plays an important role in the intergranular corrosion of Al7075 under atmospheric corrosion conditions.