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    Method of Consolidating/Molding Near Net-Shaped Components Made from Powders
    54.
    发明申请
    Method of Consolidating/Molding Near Net-Shaped Components Made from Powders 有权
    由粉末制成的网状组件附近的固化/成型方法

    公开(公告)号：US20140219854A1

    公开(公告)日：2014-08-07

    申请号：US13758609

    申请日：2013-02-04

    申请人： The Boeing Company

    发明人： Marc R. Matsen ,  Mark Alan Negley ,  Robert James Miller

    IPC分类号： B22F3/16 ,  H05B6/02

    CPC分类号： H05B6/101 ,  B21D21/00 ,  B22F3/03 ,  B22F3/087 ,  B22F3/105 ,  B22F3/14 ,  B22F3/16 ,  B22F2003/1053 ,  B22F2202/05 ,  B22F2202/07 ,  B22F2203/00 ,  C21D1/18 ,  C21D1/42 ,  C21D6/00 ,  C21D9/42 ,  H05B6/06 ,  H05B6/08 ,  H05B6/105 ,  H05B2206/023 ,  Y02P10/253

    摘要： A method for consolidating a pre-form made of powder, comprising: (a) placing the pre-form between smart susceptors; (b) heating the smart susceptors to a leveling temperature by applying a varying low-strength magnetic field having a magnetic flux that passes through surfaces of the smart susceptors; (c) applying consolidation pressure to the pre-form at least during a time period subsequent to the temperature of the smart susceptors reaching the leveling temperature; and (d) while consolidation pressure is being applied, applying a pulsed high-strength magnetic field having a magnetic flux that passes through a surface of the pre-form. The strength and pulse rate of the high-strength magnetic field are selected so that the crystallographic phase of the pre-form will rapidly oscillate at a substantially constant temperature. The pulsed high-strength magnetic field is applied sufficiently long that superplasticity of the pre-form is attained during phase oscillation.

    摘要翻译： 一种用于固结由粉末制成的预制件的方法，包括：（a）将所述预成型件置于智能基座之间; （b）通过施加具有穿过所述智能基座的表面的磁通量的变化的低强度磁场，将所述智能感受器加热到平整温度; （c）至少在智能感受器的温度达到调平温度之后的一段时间内对固化压力施加固化压力; 和（d）在施加固结压力的同时，施加具有穿过预成型件表面的磁通量的脉冲高强度磁场。 选择高强度磁场的强度和脉冲速率，使得预成型体的结晶相在基本恒定的温度下快速振荡。 脉冲高强度磁场施加足够长，使得在相位振荡期间获得预制件的超塑性。

    Composite material with a ballistic protective effect
    55.
    发明授权
    Composite material with a ballistic protective effect 有权
    复合材料具有弹道保护作用

    公开(公告)号：US08545993B2

    公开(公告)日：2013-10-01

    申请号：US12436415

    申请日：2009-05-06

    申请人： Jens-Ulrik Becker ,  Harald Hofmann ,  Christian Höckling ,  Andreas Kern ,  Udo Schriever ,  Horst Walter Tamler ,  Hans-Joachim Tschersich

    发明人： Jens-Ulrik Becker ,  Harald Hofmann ,  Christian Höckling ,  Andreas Kern ,  Udo Schriever ,  Horst Walter Tamler ,  Hans-Joachim Tschersich

    IPC分类号： F41H5/06 ,  B32B15/18

    CPC分类号： F41H5/045 ,  B32B15/011 ,  C21D9/42

    摘要： A composite material with a ballistic protective effect having a first, outer layer made of a first steel alloy and at least one second layer which is arranged under the first layer and is made of a second steel alloy. The composite material with a ballistic protective effect allows for a reduction in the weight or the wall thicknesses of the composite material in comparison to conventional composite ballistic materials, by utilizing a first steel alloy of the first layer that has the following alloy constituents in percent by weight (% by weight): 0.06%≦C ≦1.05%, 0.05%≦Si≦1.65%, 0.3%≦Mn≦2.65%, 0.015%≦Al≦1.55%; Cr≦1.2%, Ti≦0.13%, Mo≦0.7%, Nb≦0.1%, B≦0.005%, P≦0.08%, S≦0.01%, Ni≦4.0%, and V≦0.05%, the remainder being Fe and inevitable impurities. The second layer of the composite material having a higher elongation than the first layer.

    摘要翻译： 一种具有防弹效果的复合材料，具有由第一钢合金制成的第一外层和至少一个第二层，该第二层布置在第一层下方并由第二钢合金制成。 具有弹道保护作用的复合材料与传统的复合材料弹道材料相比，能够减少复合材料的重量或壁厚，通过利用具有以下合金成分的第一层的第一钢合金的百分比乘以 重量（重量％）：0.06％@ C @ 1.05％，0.05％@ Si @ 1.65％，0.3％@ Mn @ 2.65％，0.015％@ Al @ 1.55％ Cr@1.2%，Ti@0.13%，Mo@0.7%，Nb@0.1%，B@0.005%，P@0.08%，S@0.01%，Ni@4.0%，V@0.05%，其余为Fe 和不可避免的杂质。 复合材料的第二层具有比第一层高的伸长率。

    Method for manufacturing of vehicle armor components requiring severe forming with very high bend angles with very thick gauge product of high strength heat treatable aluminum alloys
    60.
    发明申请
    Method for manufacturing of vehicle armor components requiring severe forming with very high bend angles with very thick gauge product of high strength heat treatable aluminum alloys 审中-公开
    用高强度可热处理铝合金的非常厚规格的产品制造需要严格成型的车辆装甲部件的方法

    公开(公告)号：US20120261039A1

    公开(公告)日：2012-10-18

    申请号：US13385816

    申请日：2012-03-07

    申请人： Alex Cho

    发明人： Alex Cho

    IPC分类号： C22F1/04

    CPC分类号： C22F1/057 ,  C21D9/42 ,  C22F1/053

    摘要： It has been commonly believed that very thick gauge high strength aluminum alloy product such as AA2139 plate cannot be formed to the required sharp angles to form the highly protective underbody armor for the MRAP vehicles. The present process and method of manufacture provides a means for strategically combining the metallurgical process of manufacturing high strength aluminum alloys and the forming process of V shaped hull to improve the formability of the very thick gauge high strength alloy product so much that even the very thick gauge (thicker than 1 inch) plate can be formed to severe forming angles. This combined process allowed successful manufacturing of high performance V shaped hulls for the Mine Resistant Ambush Protected (MRAP) vehicles.

    摘要翻译： 通常认为，非常厚的高强度铝合金产品如AA2139板不能形成所需的锐角，以形成用于MRAP车辆的高度保护性的底部装甲。 本发明的方法和制造方法提供了一种用于战略性地组合制造高强度铝合金的冶金工艺和V形船体的成形工艺的手段，以提高非常厚厚的高强度合金产品的成形性，使得即使是非常厚的 规格（厚于1英寸）的板可以形成为严重的成形角。 这种组合过程允许成功制造用于防雷型伏击保护（MRAP）车辆的高性能V型船体。