• Title/Summary/Keyword: Mechanical properties of 6061

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Mechanical Properties of 6061Al Extruded Composite with Ti-Ni-Cu Fabricated by Ball milling (Ball milling을 이용하여 제조된 6061Al기지 Ti-Ni-Cu 압출재의 기계적특성)

  • 안인섭;배승열;김유영
    • Journal of Powder Materials
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    • v.6 no.4
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    • pp.270-276
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    • 1999
  • Ti-Ni-Cu alloy powders were fabricated by ball milling, and the properties of these powders were characterized. Mixed 50Ti-(50-x)Ni-xCu powders of 5 to 10at.%Cu composition were milled for 100 hours using SUS 1/4" balls in argon atmosphere. Ball to powder ratio was 20:1 and rotating speed was 100 rpm. Tensile strength, microstructure and phase transformation of ball milled Ti-(50-x)Ni-xCu powders were studied. After 100 hours milling, Ti, Ni and Cu elements were alloyed completely and an amorphous phase was formed. Amorphous phase was crystallized to martensite(B 19') and austenite(B2) after heat treatment for 1 hour at $850^{\circ}C$. As the Cu contents were increased, tensile strength of extruded 6061Al/TiNiCu was decreased, and B19'martensite phases In the TiNi particles were the causes of high tensile stress of extruded 6061Al/TiNiCu.NiCu.

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Effect of process type and heat treatment conditions on warm hydroformability (온간액압성형특성에 미치는 압출제조공정과 열처리 조건의 영향)

  • Yi, H.K.;Kwon, S.O.;Park, H.K.;Yim, H.S.;Lee, Y.S.;Moon, Y.H.
    • Proceedings of the Korean Society for Technology of Plasticity Conference
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    • 2007.10a
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    • pp.132-135
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    • 2007
  • In this study, hydroformability and mechanical properties of pre- and post- heat treated Al6061 tubes at different extrusion type were investigated. For the investigation, as-extruded, full annealed and T6-treated Al6061 tubes at different extrusion type were prepared. To evaluate the hydroformability, uni-axial tensile test and free bulge test were performed at room temperature and $250^{\circ}C$. Also mechanical properties of hydroformed part at various pre- and post-heat treatments were estimated by tensile test. And the tensile test specimens were obtained from hexagonal prototype hydroformed tube at $250^{\circ}C$. As for the heat treatment, hydroformability of full annealed tube is 25% higher than that of extruded tube. The tensile strength and elongation were more than 330MPa and 12%, respectively, when hydroformed part was post-T6 treated after hydroforming of pre- full annealed tube. However, hydroformed part using T6 pre treated tube represents high strength and low elongation, 8%. Therefore, the T6 treatment after hydroforming for as-extruded tube is cost-effective. Hydroformability of Al6061 tube showed similar value for both extrusion types. But flow stress of seam tube showed $20{\sim}50MPa$ lower value.

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The Fatigue Crack Growth Behavior of Silicon Carbide Particles Reinforced Aluminun Metal Matrix Composites (SiC 입자 보강 Al 복합재료의 피로균열 진전거동)

  • 권재도;문윤배;김상태
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.1
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    • pp.122-131
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    • 1995
  • The research trends for metal matrix composites have been on basic mechanical properties, fatigue behavior after aging and fractographic observations. In this study, the fatigue crack initiation as well as the fatigue crack growth behavior and the fracture mechanism were investigated through observations of the fracture surface on silicon carbide particles reinforced aluminum metal matrix composites(SiCp/Al). Based on the fractographic study done by scanning electron microscope and replica, crack growth path model and fracture mechanism are presented. The mechanical properties, such as the tensile strength, yield strength and elongation of SiCp/Al composites are improved in a longitudinal direction, however, the fatigue life is shorter than the basic Al6061 alloys. From fractographic observations, it is found that the failure mode is ductile in basic Ai6061 alloys. And because some SiC particles were pulled out from the matrix and a few SiC particles could be seen on the fracture surface of SiCp/Al, crack growth paths are believed to follow the interface of the matrix and its particles.

Evaluation of Mechanical Properties according to Anodized Coating Thickness of Aluminum Alloy for Phylon Molds (파이런 금형용 알루미늄 합금의 양극산화 코팅두께에 따른 기계적 특성 평가)

  • Kim, Tae-Wan
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.20 no.2
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    • pp.120-125
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    • 2021
  • Phylon molds are widely used for injection molding of foams used in shoe outsoles. Injection pylon molds are usually prepared by first casting the aluminum alloy and then applying an anodized coating to improve durability. This study was carried out to examine the durability of aluminum phylon molds. The aluminum materials used in this study were A771, A6061, and AC4C, and their mechanical properties were compared. Specimens for anodic oxidation tests were prepared with coating thicknesses of approximately 10 and 40 ㎛. We tried to select the optimum material and coating thickness suitable for fabricating phylon injection molds. Among the three materials, A6061 exhibited the best tensile, wear, and impact properties. The difference in the wear resistance between the soft- and hard-anodized coatings was insignificant.

Process and Mechanical Properties of Smart 6061Al Matrix Composite by Vacuum Hot Pressing (Vacuum Hot Pressing에 의한 6061Al기지 지적복합재료의 제조 및 기계적 특성)

  • Lee, Jun-Hui;Hamada, K.;Taya, M.;Inoue, K.;Park, Chang-Seon;Kim, Sun-Guk
    • Korean Journal of Materials Research
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    • v.7 no.11
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    • pp.951-956
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    • 1997
  • Vacuum Hot Pressing을 이용하여 제조한 TiNi형상기억섬유 강화 6061 AI기지 복합재료를 제조하고 미세조직 및 기계적 특성 등을 연구하였다. 제조된 복합재의 항복응력은 예비변형량, 섬유체적율 및 열처리에 따라 증가하였다. 복합재의 지적특성은 예비변형이 가하여진 후 재가열되었을 때 기지 내 TiNi 섬유의 형상기억효과에 의한 압축잔류응력 발생에 기인된다. 미세조직 관찰 섬유와 기지 사이에는 AI$_{3}$Ti및 AI$_{3}$Ni의 금속간화합물층이 관찰되었다. 또한 시험온도 증가와 더불어 TiNi섬유강화된 복합재의 유동강도는 높은 값을 나타내었다.

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Study on Multi-stage Hot Forming of A6061 Aluminum Alloy (A6061 알루미늄 합금의 다단 열간성형에 관한 연구)

  • R. H. Kim;M. H. Oh;Y. S. Jeong;S. M. Son;M. Y. Lee;J. H. Kim
    • Transactions of Materials Processing
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    • v.33 no.3
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    • pp.161-168
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    • 2024
  • Aluminum alloy sheets, compared to conventional steel sheets, face challenges in press forming due to their lower elongation. To enhance their formability, extensive research has focused on forming technologies at elevated temperatures, specifically warm forming at around 300℃ and hot forming at approximately 500℃. This study proposes that the formability of aluminum alloy sheets can be significantly enhanced using a multi-stage hot forming technique. The research also investigates whether the strength of the A6061 aluminum alloy, known for its precipitation hardening, can be maintained when formed below the precipitate solid solution temperature. In the experiments, the A6061-T6 sheet underwent heating and rapid cooling between 250 and 500℃. The mechanical properties were evaluated at each stage of the process. The findings revealed that when the initial heat treatment was below 350℃, the strength of the material remained unchanged. However, at temperatures above 400℃, there was a noticeable decrease in strength coupled with an increase in elongation. Conversely, when the secondary heat treatment was conducted at temperatures of 350℃ or lower, the strength remained comparable to that of the initial heat treated material. However, at higher temperatures, a reduction in strength and an increase in elongation were observed.

Fabrication and Interface Properties of TiNi/6061Al Composite (TiNi 형상기억합금을 이용한 복합재료의 제조 및 계면 특성)

  • Kim, Sun-Guk;Lee, Jun-Hui
    • Korean Journal of Materials Research
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    • v.9 no.4
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    • pp.419-427
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    • 1999
  • TiNi shape memory alloy was shape memory heat-treated and investigated its mechanical properties with the variation of prestrain. Also 6061 Al matrix composites with TiNi shape memory alloy fiber as reinforcement have been fabricated by Permanent Mold Casting to investigate the microstructures and interface properties. Yield stress of TiNi wire was the most high in the case of before heat-treatment and then decreased as increasing heat-treatment time. In each heat-treatment condition, the yield stress of TiNi wire was not changed with increasing the amount of prestrain. The interface bonding of TiNi/6061Al composite was fine. There was a 2$\mu\textrm{m}$ thickness of diffusion reaction layer at the interface. We could find out that this diffusion reaction layer was made by the mutual diffusion. The diffusion rate from Al base to TiNi wire was faster than that of reverse diffusion and the amount of the diffusion was also a little more than that of reverse.

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The Effect of Solution Heat Treatment and Aging Treatment on the Mechanical Properties of Backward Extruded A6061 Alloy for Pressure Vessels (고압용기로 사용되는 후방압출된 알루미늄 6061합금의 기계적 특성에 미치는 용체화처리 및 시효처리의 영향)

  • Kwon, Eui Pyo;Woo, Kee Do;Moon, Min Seok;Kang, Duck Soo;Nam, Gung Cheon;Yoo, Gye Hyoung
    • Korean Journal of Metals and Materials
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    • v.47 no.3
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    • pp.175-181
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    • 2009
  • Mechanical properties and precipitation behavior of backward extruded 6061 Al alloy for pressure vessel were investigated using tensile test, transmission electron microscopy (TEM) and differential scanning calorimeter (DSC). In this study, solution heat treatment (SHT) was performed at $535^{\circ}C$ for 30~90 min and aging treatment was conducted at 177 and $190^{\circ}C$ for 1~7 h. Maximum tensile strength of $36.6kgf/mm^2$ and yield strength of $33.29kgf/mm^2$ were achieved at the aging time of 5 h at $190^{\circ}C$. TEM observation showed that fine needle-like ${\beta}^{{\prime}{\prime}}$ phase which has 35~45 nm of length was uniformly distributed in the aged 6061 Al alloy specimen. From tensile test, TEM and DSC analysis, it is expected that aging time of 2~5 h at $190^{\circ}C$ is suitable for the extruded A6061 used as pressure vessels.

Effect of Ball milling Time on Graphite Dispersion and Mechanical Properties in Rapidly Solidified 6061 Al Composite (급속응고 6061Al/Graphite 복합재료의 볼밀링 시간에 따른 흑연 분산거동 및 기계적 특성)

  • Son, Hyeon-Taek;Lee, Jae-Seol;Hong, Soon-Jik;Chun, Byong-Sun
    • Journal of Powder Materials
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    • v.16 no.3
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    • pp.209-216
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    • 2009
  • A composite of rapidly solidified Al-6061 alloy powder with graphite particle reinforcements was prepared by ball milling and subsequent hot extrusion. The microstructure and mechanical properties of these composites were investigated as a function of milling time. With increasing milling time, the gas atomized initially and spherical powders became elongated with a maximum aspect ratio after milling for 30 h. Then, refinement and spheroidization were achieved by further milling to 70 h with a homogeneous and fine dispersion of graphite particles forming between the matrix alloy layers. The best compression and wear properties were obtained in the powder milled for 70 h, associated with the increased fine and homogeneous distribution of graphite particles in the aluminum alloy matrix.

An Analysis on the Forging Processes for 6061 Aluminum Alloy Wheel (6061 알루미늄합금 휠 단조공정의 해석)

  • 김영훈;유태곤;황병복
    • Transactions of Materials Processing
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    • v.8 no.5
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    • pp.498-506
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    • 1999
  • The metal forming processes of aluminum alloy wheel forging at elevated temperature are analyzed by the finite element method. A coupled thermo-mechanical model for analysis of plastic deformation and geat transfer is adapted in the finite element formulation. In order to consider the strain-rate effects on material properties and the flow stress dependence on temperatures, rigid-viscoplasticity is introduced in this formation. In this paper, several process conditions were applied to the dimulation such as die speed, rib thickness, and depth of die cavity. Simulation results are compared, and discussed with each case. Metal flow, die pressure distributions, temperature distributions, velocity fields and forging loads are summarized as basic data for process design and selection of a proper press equipment.

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