• 제목/요약/키워드: 7050

검색결과 48건 처리시간 0.02초

7050 Al합금의 응력부식저항성에 미치는 2단 시효처리의 영향 (Effect of Two-Step Aging Treatment on the Stress Corossion Cracking Resistance of 7050 Al Alloy)

  • 최중환;김종기;김헌규;이상래;김인배
    • 한국재료학회지
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    • 제9권7호
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    • pp.695-700
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    • 1999
  • 7050 Al합금의 응력부식저항성에 미치는 2단 시효처리의 영향을 미세조직관찰, 전기전도도시험 및 SCF값을 평가함으로써 조사하였다. 최대 경도 이상 과시효에 의해 주 강화상인 η'상이 η상으로 변태되었고, 입내 및 입계에 존재하는 η상의 크기와 간격이 커졌으며 그 결과 응력부식저항성이 증대되었다. 2차 시효시간의 증가에 따라 전기전도도값은 증가되었으나 항복강도의 감소로 인하여 SCF값은 감소되었는데, 이러한 결과는 응력부식저항성의 증가를 의미한다. AMS 4107규격을 기준으로 하였을 때 7050 Al합금 단조재의 적정시효조건은 1차시효가 12$0^{\circ}C$에서 6시간, 2차시효는 $175^{\circ}C$에서 12시간이었다.

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항공기용 Al 합금 단조품의 특성 향상을 위한 단조 공정 설계 (Forging Process Design to Improve the Properties of Al Alloy Forged Part for Aerospace)

  • 이영선;이정환
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2001년도 추계학술대회 논문집
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    • pp.228-232
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    • 2001
  • Fatigue strength, electrical conductivity and stress-corrosion-cracking resistance are considered as important factors at aircraft Al alloys, therefore Al7050 alloy has been developed to improve such properties. However, hammer-forged Al7050 parts showed the undesirable structures such as severe local grain coarsening and inhomogeneous material flow, resulted in the degraded mechanical properties. 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 The use of preform has been beneficial for reduction of the forging load and elimination of the grain coarsening. However, in the cases 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.

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

  • 이창우;권숙인
    • 열처리공학회지
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    • 제7권4호
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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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Lateral growth of PEO films on Al7050 alloy in 0.1 M NaAlO2

  • Moon, Sungmo;Kim, Gi Yeob
    • 한국표면공학회지
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    • 제54권4호
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    • pp.200-208
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    • 2021
  • This paper investigated generation behavior of micro-arcs and growth behavior of PEO films on the AA7050 disc specimen in 0.1 M NaAlO2 solution under the application of 1200 Hz anodic pulse current. Morphologies, thickness and surface roughness of PEO films were examined at the edge part and central part separately. Micro-arcs were generated first at the edge part and then moved towards the central part with PEO treatment time, indicating lateral growth of PEO films. The lateral growth resulted in uniform PEO thickness of about 5 ㎛ and surface roughness of about 0.5 ㎛. Moving of the arcs from the edge towards the central part appeared only one time and large size arcs were generated at the edge before completing the central part with small size micro-arcs. This suggests that vertical growth starts before completing the lateral growth. Large size arcs generated at the edge resulted in the formation of relatively large size pores within the PEO films on the AA7050 disc specimen.

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

  • 김문호;권숙인
    • 열처리공학회지
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    • 제4권4호
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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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7050 Al합금의 미세조직 및 기계적성질에 미치는 시효처리의 영향 (Effect of Aging Treatment on the Microstructures and Mechanical Properties of 7050 Al Alloy)

  • 김종기;최중환;김인배;김종기;이상래
    • 한국재료학회지
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    • 제7권9호
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    • pp.789-794
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    • 1997
  • 7050AI합금의 미세조직 및 기계적성질에 미치는 2단시효처리의 영향을 투과전자현미경, 열분석, 경도시험 및 인장 시험을 통하여 조사하였다. 12$0^{\circ}C$에서 6시간 1차 시효처리한 후 1$65^{\circ}C$와 175$^{\circ}C$에서 2차 시효처리하였을때 1$65^{\circ}C$에서는 6시간 시효시 최대경도값 201.3Hv를 나타내었고, 175$^{\circ}C$에서는 3시간 시효처리하였을때 최대경도값 197Hv를 나타내었다.

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

  • 배동화;오주희;정찬욱;김정기
    • 소성∙가공
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    • 제31권2호
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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.