Aluminum alloy semi-ring for fairing of launch vehicle and preparation method thereof
A technology for launch vehicles and aluminum alloys, which is used in metal extrusion control equipment, metal processing equipment, metal extrusion, etc. The effect of processing plasticity and reducing dimensional deformation
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specific Embodiment approach 1
[0012] Embodiment 1: The aluminum alloy half ring for the launch vehicle fairing of the present embodiment is composed of 0.6% to 1.2% of Si, 0.1% to 0.7% of Fe, 3.9% to 4.8% of Cu, and 0.4% to 1.0% by mass percentage. % of Mn, 0.4% to 0.8% of Mg, 0.05% to 0.1% of Ni, 0.1% to 0.3% of Zn, 0.1% to 0.15% of Ti and 90.95% to 94.35% of Al.
[0013] The tensile strength of aluminum alloy half rings for launch vehicle fairings is 380MPa~450MPa, the elongation after fracture is 6.0%~10%, and the Brinell hardness (HB) is 110N / mm 2 ~150N / mm 2 , which can meet the strength requirements of large launch vehicles.
specific Embodiment approach 2
[0014] Specific embodiment 2: The difference between this embodiment and specific embodiment 1 is that the aluminum alloy half ring for the launch vehicle fairing consists of 0.8% to 1.1% Si, 0.2% to 0.6% Fe, 4.0% to 4.6% by mass percentage % Cu, 0.5% to 0.9% of Mn, 0.5% to 0.7% of Mg, 0.06% to 0.08% of Ni, 0.15% to 0.25% of Zn, 0.11% to 0.14% of Ti and 91.63% to 93.68% of Al made.
specific Embodiment approach 3
[0015] Specific embodiment three: the difference between this embodiment and specific embodiment one or two is that the aluminum alloy half ring for the launch vehicle fairing consists of 1.0% Si, 0.4% Fe, 4.3% Cu, and 0.7% Made of Mn, 0.6% Mg, 0.07% Ni, 0.20% Zn, 0.13% Ti and 92.60% Al.
[0016] The tensile strength of the aluminum alloy half ring for the launch vehicle fairing of this embodiment is 402MPa, the elongation after fracture is 6.5%, and the Brinell hardness (HB) is 140N / mm 2 , which can meet the strength requirements of large launch vehicles.
[0017] Specific embodiment three: the preparation method of the aluminum alloy half-ring for the launch vehicle fairing of the present embodiment is carried out according to the following steps: 1. According to the mass percentage Si of elements in the aluminum alloy half-ring for the launch vehicle fairing: 0.6%~1.2% , Fe: 0.1%~0.7%, Cu: 3.9%~4.8%, Mn: 0.4%~1.0%, Mg: 0.4%~0.8%, Ni: 0.05%~0.1%, Zn: 0.1%~0.3%, Ti Al: 0.1%...
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