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Method of shaping a semi-finished product on a hammer, in particular for producing an aerospace fastener
Method of shaping a semi-finished product on a hammer, in particular for producing an aerospace fastener
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机译:在锤上成型半成品的方法,特别是用于制造航空航天紧固件的方法
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摘要
The method of shaping on a semi-finished hammer, in particular for the manufacture of air anchorages, consists of the upper (1) and lower (3) matrices having working patterns in the middle (1a and 3a),heated in the kiln and using gas burners to 250oC temperature and placed on a punching hammer with the energy of impact 36 kJ and the mass of the kiln 1000 kg, after which the feed material in the form of a moulded pre-cap cast in sand form with less plastic aluminium alloys of the aluminium-copper group is heated in the kiln in temperature range 460-500-C, preferably 480-C, up to fifty minutes, then the heated input material is placed in the working range (3a) of the lower matrix (3),Then the top matrix (1) moves progressively up to 10 m/s in the direction of the bottom matrix (3) and the input material is crushed with the working pattern (1a) of the top matrix (1) and the working pattern (3a) of the bottom matrix (3) and the semi-finished product (2b) is formed with a greater degree of conversion.
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机译:在半成品锤上成型的方法,特别是用于制造空气锚点的方法,由上部(1)和下部(3)矩阵组成,它们在中间(1a和3a)中具有工作模式,并在窑炉中加热。使用气体燃烧器将温度升高到250oC,并放置在冲击能量为36 kJ,窑质量为1000 kg的打孔锤上,然后将原料以模制的预盖形式浇铸成砂型,并减少塑料铝的含量将铝-铜族合金在窑炉中在460-500-C,最好是480-C的温度范围内加热长达五十分钟,然后将加热的输入物料置于下基体的工作范围(3a)中( 3),然后顶部矩阵(1)逐渐沿底部矩阵(3)的方向移动高达10 m / s,输入材料被顶部矩阵(1)的工作模式(1a)和底部基质(3)和半成品(2b)的加工图案(3a)形成的程度更大。转换。
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