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    • 7. 发明申请
    • METHOD FOR SUPERPLASTIC FORMING OF RAPIDLY SOLIDIFIED MAGNESIUM BASE METAL ALLOYS
    • 快速固化镁基金属合金超塑性成型方法
    • WO1991013181A1
    • 1991-09-05
    • PCT/US1991001048
    • 1991-02-18
    • ALLIED-SIGNAL INC.
    • ALLIED-SIGNAL INC.DAS, Santosh, K.CHANG, Chin-FongRAYBOULD, Derek
    • C22C01/04
    • C22F1/06B22F3/006C22C1/0408C22C23/02Y10S420/902
    • A complex part composed of rapidly solidified magnesium base metal alloy is produced by superplastic forming at a temperature ranging from 160 DEG C to 275 DEG C and at a rate ranging from 0.00021 m/sec to 0.00001 m/sec, to improve the formability thereof and allow forming to be conducted at lower temperature. The rapidly solidified magnesium based alloy has a composition consisting essentially of the formula MgbalAlaZnbXc, wherein X is at least one element selected from the group consisting of manganese, cerium, neodymium, praseodymium and yttrium, ''a'' ranges from 0 to about 15 atom percent, ''b'' ranges from 0 to about 4 atom percent and ''c'' ranges from about 0.2 to 3 atom percent, the balance being magnesium and incidental impurities, with the proviso that the sum of aluminum and zinc present ranges from about 2 to 15 atom percent. Such an alloy contains fine grain size and finely dispersed magnesium-, aluminum- rare earth intermetallic phases. When formed, the part exhibits good corrosion resistance together with high ultimate tensile strength and good ductility at room temperature, which properties are, in combination, far superior to those of conventional magnesium alloys. The part is suitable for application as a structural member in helicopters, missiles and air frames where good corrosion resistance in combination with high strength and ductility is important.
    • 由快速凝固的镁基金属合金构成的复合部分通过在160℃至275℃的温度范围内以0.00021m / sec至0.00001m / sec的速率超塑性生产,以提高其成型性, 允许成形在较低温度下进行。 快速凝固的镁基合金具有基本由式MgbalAlaZnbXc组成的组成,其中X是选自锰,铈,钕,镨和钇中的至少一种元素,“a”的范围为0至约15 原子百分比,“b”的范围为0至约4原子百分数,“c”为约0.2至3原子%,余量为镁和附带杂质,条件是铝和锌的总和存在 范围为约2至15原子%。 这种合金含有细晶粒度和细分散的镁,铝 - 稀土金属间相。 当形成时,该部件在室温下表现出良好的耐腐蚀性以及高极限拉伸强度和良好的延展性,其组合远远优于传统的镁合金。 该部件适用于作为直升机,导弹和空气框架中的结构构件,其具有良好的耐腐蚀性以及高强度和延展性的重要性。
    • 8. 发明申请
    • DUAL PROCESSING OF ALUMINUM BASE ALLOYS
    • 铝基合金的双加工
    • WO1991007513A2
    • 1991-05-30
    • PCT/US1990003608
    • 1990-06-26
    • ALLIED-SIGNAL INC.
    • ALLIED-SIGNAL INC.DAS, Santosh, K.ZEDALIS, Michael, S.GILMAN, Paul, S.
    • C22C0
    • C22C1/1084B22F2998/10C22C32/0052B22F9/008B22F1/0003B22F9/04
    • An aluminum based alloy is produced from a charge containing a rapidly solidified aluminum alloy and a carbidiferous agent in an amount ranging from about 0.01 to 10 % by weight of the charge. The charge is ball milled energetically to uniformly mix the carbidiferous agent within the aluminum base alloy while maintaining the charge in a pulverulent state. Upon completion of the ball milling step, the charge is hot consolidated at suitable temperatures to react the carbidiferous agent with the aluminum base alloy, resulting in the formation of carbide and oxide particles, and to provide a powder compact having a formable, substantially void-free mass. The compact is especially suited for use in aerospace, automotive, electronic, strength critical components, and the like, which often encounter service temperatures approaching 500 DEG C.
    • 由含有快速固化的铝合金和含碳化合物的电荷产生铝基合金,其量为电荷的约0.01至10重量%。 将电荷球磨以均匀混合铝基合金中的碳化物,同时保持电荷处于粉状状态。 在球磨步骤完成后,将电荷在合适的温度下热固化以使含碳化合物与铝基合金反应,导致碳化物和氧化物颗粒的形成,并提供具有可成形的, 自由质量 该紧凑件特别适用于经常遇到接近500℃的使用温度的航空航天,汽车,电子,强度关键部件等。