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公开(公告)号：USD413589S
公开(公告)日：1999-09-07
申请号：US93936
申请日：1998-09-22
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公开(公告)号：USD412896S
公开(公告)日：1999-08-17
申请号：US93926
申请日：1998-09-22
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公开(公告)号：US20110196099A1
公开(公告)日：2011-08-11
申请号：US13091777
申请日：2011-04-21
CPC分类号： B01J13/0043
摘要： Methods of producing a plurality of particle aggregates having a specified number of member particles are provided according to embodiments of the present invention. Specific methods include stimulating a plurality of particles with an aggregation stimulus to form a plurality of particle aggregates and then quenching the aggregation stimulus in order to inhibit further particle aggregation. An individual particle aggregate of the produced plurality of particle aggregates has member particles including at least a first member particle and a second member particle. Member particles of particle aggregates are optionally subjected to fusion to stabilize the particle aggregates. Produced particle aggregates having a specified number of member particles may be purified to enrich for particular aggregates.
摘要翻译： 根据本发明的实施例，提供了具有特定数量的构件颗粒的多个颗粒聚集体的制备方法。 具体方法包括用聚集刺激刺激多个颗粒以形成多个颗粒聚集体，然后淬灭聚集刺激以便抑制进一步的颗粒聚集。 所生产的多个颗粒聚集体的单个颗粒聚集体具有至少包括第一构件颗粒和第二构件颗粒的构件颗粒。 颗粒聚集体的成员颗粒任选地进行熔融以稳定颗粒聚集体。 可以纯化具有特定数目的成员颗粒的生成的颗粒聚集体以富集特定聚集体。
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公开(公告)号：US4348957A
公开(公告)日：1982-09-14
申请号：US172879
申请日：1980-07-28
CPC分类号： F42B15/38
摘要： A device for altering the after body shape of a missile configuration so aso reduce the ballistic flight drag coefficient after booster burnout and including linear shaped charge cutting device for severing a portion of a nozzle exit cone just aft of a fixed boattail configuration on the outer surface of the missile to allow boundary layer air flow to flow smoothly over the boattail and thereby reduce the base drag on the missile during the coast phase thereof.
摘要翻译： 一种用于改变导弹构造的后身体形状的装置，以便在加强器烧坏之后降低弹道飞行阻力系数，并且包括线性成形的充电切割装置，用于在外侧的固定火炬结构的后方切断喷嘴出口锥的一部分 导弹的表面，以允许边界层气流平稳地流过火炬，从而减少导弹在其海岸相期间的基地阻力。
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公开(公告)号：US4007586A
公开(公告)日：1977-02-15
申请号：US630114
申请日：1975-11-10
申请人： Joseph J. McDermott
发明人： Joseph J. McDermott
CPC分类号： F02K9/82
摘要： A spin nozzle system for imparting a thrust to pre-spin a missile prior toaunching. This system includes locating the spin nozzles within the outside diameter of the main missile motor. Also the nozzle exhaust gases are exited into the main motor exhaust cone to thereby augment the total missile thrust.
摘要翻译： 旋转喷嘴系统，用于在发射之前施加推力以预先旋转导弹。 该系统包括将旋转喷嘴定位在主导弹马达的外径内。 喷嘴废气也被排出到主电机排气锥体中，从而增加总导弹推力。
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公开(公告)号：USD412897S
公开(公告)日：1999-08-17
申请号：US93927
申请日：1998-09-22
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公开(公告)号：US20080072402A1
公开(公告)日：2008-03-27
申请号：US11858536
申请日：2007-09-20
IPC分类号： B01F3/12
CPC分类号： B01J13/0043
摘要： Methods of producing a plurality of particle aggregates having a specified number of member particles are provided according to embodiments of the present invention. Specific methods include stimulating a plurality of particles with an aggregation stimulus to form a plurality of particle aggregates and then quenching the aggregation stimulus in order to inhibit further particle aggregation. An individual particle aggregate of the produced plurality of particle aggregates has member particles including at least a first member particle and a second member particle. Member particles of particle aggregates are optionally subjected to fusion to stabilize the particle aggregates. Produced particle aggregates having a specified number of member particles may be purified to enrich for particular aggregates.
摘要翻译： 根据本发明的实施例，提供了具有特定数量的构件颗粒的多个颗粒聚集体的制备方法。 具体方法包括用聚集刺激刺激多个颗粒以形成多个颗粒聚集体，然后淬灭聚集刺激以便抑制进一步的颗粒聚集。 所生产的多个颗粒聚集体的单个颗粒聚集体具有至少包括第一构件颗粒和第二构件颗粒的构件颗粒。 颗粒聚集体的成员颗粒任选地进行熔融以稳定颗粒聚集体。 可以纯化具有特定数目的成员颗粒的生成的颗粒聚集体以富集特定聚集体。
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