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2023211 · ZL205A alloy, as a high-strength casting aluminum alloy, is frequently used in aviation, aerospace, metallurgy and transportation, 1 while the low-pressure castings
contact2019825 · The multiphase layer is prepared through a duplex treatment consisting of two steps. The first one is the deposition of Ti film on the ZL205A aluminum alloy by
contact20221126 · In this paper, ZL205A (AlCu5Mn alloy) castings were prepared by squeeze casting. The effects of solution and ageing treatment on the microstructure and
contactFig.1 Three-dimensional printing (3DP) sand mold (a) and schematics of hot tearing susceptibility testing (unit: mm) (b), and 3DP sand mold of the single-helix fluidity testing
contactIn this paper, effects of partial remelting treatment on microstructure and properties of ZL205A alloy were studied in detail. The results show that the grain size of ZL205A alloy
contact2023211 · ZL205A alloy, as a high-strength casting aluminum alloy, is frequently used in aviation, aerospace, metallurgy and transportation, 1 while the low-pressure castings play an active role in national defense construction and other industries. However, the casting is prone to flaws attributable to the mushy solidification qualities of the ZL205A alloy, 2 the
contact2019825 · The multiphase layer is prepared through a duplex treatment consisting of two steps. The first one is the deposition of Ti film on the ZL205A aluminum alloy by magnetron sputtering ion plating system (UDP-450) from Teer Coatings Ltd., UK. The high quality Ti target (99.999%, 330 mm × 134 mm × 8 mm) is utilized.
contact2018126 · : The wall of ZL205A aluminum alloy were carried out by the wire+arc additive manufacturing technology (WAAM). The microstructure,mechanical properties and so on of ZL205A aluminium alloy wall were investigated by metallographic, SEM, EDS and tensile tests, and compared with that of metal casting alloy. The results
contactFig.1 Three-dimensional printing (3DP) sand mold (a) and schematics of hot tearing susceptibility testing (unit: mm) (b), and 3DP sand mold of the single-helix fluidity testing (c) Fig.2 Schematics of the tensile specimen of 3DP sand mold (unit: mm) Fig.3 Macro-morphologies of ZL205A alloy hot tearing susceptibility bars prepared by 3DP sand mold
contact202153 · The galvanic corrosion behaviors between carbon fiber-reinforced epoxy composites (CFREC) and aluminum alloy (2219 and ZL205A) in 3.5 wt.% sodium chloride solutions were evaluated by laboratory ...
contact20161010 · ZL205A aluminum alloy as the anodic material and CFREC as the cathode material. CFREC was made of MT300/803, polyacrylonitrile based unidirectional woven carbon fiber reinforced epoxy composites, and the laminate was prepared with vacuum autoclave method. The element components of the two kinds of aluminum alloys
contact2020923 · The ZL205A aluminum alloy ingot was melted in a graphite crucible inside an electric resistance furnace. The melt was smelted and refined for five minutes with 0.8 wt % refining agent at 730 °C and then raised the temperature of molten metal to 760 °C. ... Quanta 200, FEI, Czech Republic). Energy disperse spectroscopy (EDS, Oxford INCA,
contact20221126 · In this paper, ZL205A (AlCu5Mn alloy) castings were prepared by squeeze casting. The effects of solution and ageing treatment on the microstructure and mechanical properties of ZL205A castings were studied by metallography, scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS) and mechanical properties
contact2014423 · Bending strength measurements were conducted on C f /Al composite specimens (with dimension of 4 mm × 4 mm × 36 mm) using a three-point bending fixture with a span length of 30 mm at a crosshead speed of 0.5 mm·min −1 (Fig. 3).For comparison, the bending test on the matrix aluminum alloy ZL205A specimens was also
contact2014111 · The experiments and numerical simulation were conducted for ZL205A aluminum alloy cylindrical shell casting. The formation mechanism of the linear segregation produced by the low pressure die casting (LPDC) process was investigated. And the heat transfer of the casting during solidification process was analyzed by simulation technique ...
contact2021121 · In this paper, a nanosecond fiber pulse laser is used to carry out the experimental study on laser weight removal of ZL205A aluminum alloy gyro rotor. By optimizing the process parameters of laser ...
contact2017715 · Laser cladding of homogeneous coating onto ZL205A substrate by using a high-power diode laser was investigated in order to repair casting defects of ZL205A aluminum alloy. ... Casting defects induced fatigue damage in aircraft frames of ZL205A aluminum alloy–a failure analysis. Mater. Des., 32 (2011), pp. 2570-2582. View PDF
contactSince the development of the aviation industry, improving the flight performance and reducing the weight of aircrafts has always been the goal pursued by aviation designers. Therefore, it becomes increasingly important to develop a new alloy material with high hardness, high strength, and light weight. To obtain excellent mechanical properties and
contactOx Pro Aluminium Hawk 330 x 330mm. SKU: TOX33037. Ox Pro aluminium hawk 330 x 330mm engineered for holding plaster or mortar ready for application. Manufactured from heavy gauge hard-rolled aluminium delivering strength and rigidity.
contact20191017 · Malvern UK Mastersizer 3000. The chemical composition of this powder which was measured via ICP-AES (inductive coupled plasma atomic emission spectrometry) is tabulated in Table 1. ... As AlCu5MnCdVA is a heat-treatable aluminum alloys, there are many trace strengthening phase after proper heat treatment. They are absent or little in
contact: . : : 1000. > >. 【】 ZL205A ZL116 . ￥16.5 0. ZL205A ZL108102 104 106. ￥15.8 0. / ZL205A ...
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