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    Subcaliber kinetic energy projectile
    1.
    发明授权
    Subcaliber kinetic energy projectile 失效
    亚光谱动能弹丸

    公开(公告)号：US5289777A

    公开(公告)日：1994-03-01

    申请号：US25400

    申请日：1993-02-26

    申请人： Achim Sippel ,  Heinz-Josef Kruse ,  Walter Klumpp ,  Jurgen Bocker ,  Jurgen Meyer ,  Michael Geis ,  Rolf Holl

    发明人： Achim Sippel ,  Heinz-Josef Kruse ,  Walter Klumpp ,  Jurgen Bocker ,  Jurgen Meyer ,  Michael Geis ,  Rolf Holl

    IPC分类号： F42B14/06

    CPC分类号： F42B14/061

    摘要： A subcaliber kinetic energy projectile (1) including a penetrator (2) and a segmented sabot (3) which is provided with a front support (4) and with a second support (5) that is disposed at an axial distance behind the first support, with the second support (5) including a rotationally symmetrical air pocket (6) that faces the first support (4) and the first support (4) is provided with air passage openings (43, 44, 45).In the sabot, the relationship of L/D.gtoreq.1.2 exists between the length L of the penetrator tip (8) ahead of the first support (4) and the caliber D. The relationship x.gtoreq.0.45 * .iota. further applies between the distances x and .iota., with x being the distance between the trailing edge (10) of the sabot and the base surface (11) of the air pocket (6) in the second support (5) and .iota. being the distance between the trailing edge (10) of the sabot (3) and the leading edge (12) of the sabot at the surface of the penetrator (2). Finally, the first support (4) is composed of at least three laterally extending web-like components (40-42) whose shape and dimensions are such that they form and have the effect of three separate air pockets.

    摘要翻译： 一种包括穿透器（2）和分段式破坏物（3）的亚规模动能射弹（1），其设置有前支撑件（4）和第二支撑件（5），所述第二支撑件设置在所述第一支撑件后面的轴向距离处 第二支撑件（5）包括面向第一支撑件（4）的旋转对称的气穴（6），并且第一支撑件（4）设置有空气通道开口（43,44,45）。在支架中， L / D> = 1.2之间的关系存在于第一支撑件（4）之前的穿透尖端（8）的长度L与口径D之间。关系x> = 0.45 *（iota）还应用于距离x 和（iota），其中x是在第二支撑件（5）中的破坏件的后缘（10）和气囊（6）的基部表面（11）之间的距离，并且（iota） 砧座（3）的后缘（10）和砧座的前缘（12）在穿透器（2）的表面。 最后，第一支撑件（4）由至少三个横向延伸的网状部件（40-42）组成，其形状和尺寸使得它们形成并具有三个独立气囊的作用。

    Surface-emission cathodes having cantilevered electrodes
    2.
    发明申请
    Surface-emission cathodes having cantilevered electrodes 失效
    具有悬臂电极的表面发射阴极

    公开(公告)号：US20070090476A1

    公开(公告)日：2007-04-26

    申请号：US11237637

    申请日：2005-09-28

    申请人： Michael Geis ,  Theodore Fedynyshyn ,  Sandra Deneault ,  Keith Krohn ,  Theodore Lyszczarz ,  Michael Marchant

    发明人： Michael Geis ,  Theodore Fedynyshyn ,  Sandra Deneault ,  Keith Krohn ,  Theodore Lyszczarz ,  Michael Marchant

    IPC分类号： H01L29/84

    CPC分类号： H01J1/304 ,  H01J1/32

    摘要： A surface-emission cathode formed on an insulating surface having cantilevered, i.e. “undercut,” electrodes. Suitable insulating surfaces include negative electron affinity (NEA) insulators such as glass or diamond. The cathode can operate in a comprised vacuum (e.g., 10−7 Torr) with no bias on the electrodes and low vacuum electric fields (e.g., at least 10 V cm−1). Embodiments of the present invention are inexpensive to fabricate, requiring lithographic resolution of approximately 10 micrometers. These cathodes can be formed over large areas for use in lighting and displays and are suitable for satellite applications, such as cathodes for tethers, thrusters and space-charging neutralizers.

    摘要翻译： 形成在具有悬臂的绝缘表面上的表面发射阴极，即“底切”电极。 合适的绝缘表面包括负电子亲和力（NEA）绝缘体，如玻璃或金刚石。 阴极可以在电极和低真空电场（例如，至少10V cm -1 -1以上）没有偏压的情况下在包含的真空（例如，10 -7托）中操作 >）。 本发明的实施例制造成本低廉，需要约10微米的光刻分辨率。 这些阴极可以形成在用于照明和显示器的大面积上，并且适用于卫星应用，例如系绳阴极，推进器和空间充电中和剂。