Alloy material for aircraft seat framework
An alloy material and aircraft seat technology, applied in the field of aluminum-based alloys, can solve the problems of frequent use, easy damage, and a large amount of passenger seats in civil aviation, and achieve the effect of excellent compression resistance and high hardness
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[0031] Example 1
[0032] Raw material composition:
[0033] Ti: 0.30%, Mn: 0.85%, P: 0.025%, Cu: 0.04%, Si: 0.45%, Cr: 13.0%, Ni: 7.0%, Zn: 0.18%, V: 0.27%, Co: 0.02%, W: 0.03%, Ce: 0.25%, Lu: 0.20%, and the rest is Al.
[0034] Prepared by the following method:
[0035] Put the elements of Al, Ti, Mn, P, Cu, Si, Cr, Ni, Zn, V, Co, W to be smelted into the vacuum chamber of the water-cooled copper crucible, evacuate, melt the elements, and then add Ce, Lu, Al elementary substance, heat preservation for 10 min, stir evenly, use centrifugal casting method to cast aircraft seat frame alloy material at 500℃, centrifugal speed 400rpm conditions, complete in 6 seconds; at 800℃, hot isostatic pressure 180MPa conditions , Keep the pressure for 2 hours to obtain the finished aircraft seat frame alloy material.
Example Embodiment
[0036] Example 2
[0037] Raw material composition:
[0038] Ti: 0.21%, Mn: 0.5%, P: 0.02%, Cu: 0.02%, Si: 0.25%, Cr: 12.0%, Ni: 3.0%, Zn: 0.13%, V: 0.2%, Co: 0.01%, W: 0.02%, Ce: 0.15%, Lu: 0.15%, and the rest is Al.
[0039] Prepared by the following method:
[0040] Put the elements of Al, Ti, Mn, P, Cu, Si, Cr, Ni, Zn, V, Co, W to be smelted into the vacuum chamber of the water-cooled copper crucible, evacuate, melt the elements, and then add Ce, Lu, Al simple substance, heat preservation for 15 minutes, stir evenly, use centrifugal casting method to cast aircraft seat frame alloy material at 550℃, centrifugal speed 450rpm conditions, complete in 8 seconds; at 850℃, hot isostatic pressure 190MPa conditions, After holding the pressure for 2.5 hours, the finished aircraft seat frame alloy material is obtained.
Example Embodiment
[0041] Example 3
[0042] Raw material composition:
[0043] Ti: 0.35%, Mn: 1.05%, P: 0.03%, Cu: 0.05%, Si: 0.55%, Cr: 15.0%, Ni: 9.0%, Zn: 0.21%, V: 0.3%, Co: 0.03%, W: 0.04%, Ce: 0.30%, Lu: 0.30%, the rest is Al.
[0044] Prepared by the following method:
[0045] Put the elements of Al, Ti, Mn, P, Cu, Si, Cr, Ni, Zn, V, Co, W to be smelted into the vacuum chamber of the water-cooled copper crucible, evacuate, melt the elements, and then add Ce, Lu, Al elementary substance, heat preservation for 20min, stir evenly, use centrifugal casting method to cast aircraft seat frame alloy material at 600℃, centrifugal speed 500rpm conditions, complete in 10 seconds; at 900℃, hot isostatic pressure 210MPa conditions, After holding the pressure for 3 hours, the finished aircraft seat frame alloy material is obtained.
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