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    • 2. 发明授权
    • Spin stabilized projectile unit
    • 旋转稳定的射弹单元
    • US5090328A
    • 1992-02-25
    • US749705
    • 1991-08-26
    • Ulrich TheisH. -P. HellmeisterBernhard BispingMichael VagedesSiegfried KeblerHorst KantnerPeter Sommer
    • Ulrich TheisH. -P. HellmeisterBernhard BispingMichael VagedesSiegfried KeblerHorst KantnerPeter Sommer
    • F42B14/06
    • F42B14/064
    • A spin stabilized projectile unit includes a sub-caliber projectile having a cylindrical section connected to a conical tail section including an external circumferential holding groove. A propelling cage casing encloses the projectile. A propelling base includes a receptacle holding the projectile and connected with the projectile and the propelling cage casing. The receptacle includes inwardly projecting axial webs presenting an inner diameter of the receptacle in a region of the cylindrical section of the projectile which corresponds to the outer diameter of the cylindrical section. The inner diameter of the receptacle formed by the webs becomes increasingly larger than the respective outer diameter of the conical section beginning in the transition region between the cylindrical and conical sections to form an annular gap extending to a bottom region of the bottom of the receptacle. A segmented holding ring is disposed between the inner diameter of the receptacle and the outer diameter of the conical tail section and lies in the holding groove and against the inner diameter of the receptacle for holding the projectile in the receptacle of the propelling base.
    • 旋转稳定的射弹单元包括具有连接到包括外部周向保持槽的锥形尾部的圆柱形部分的子口径射弹。 一个推进的笼罩包围着弹丸。 推进基座包括容纳弹丸并与射弹和推进笼壳连接的容器。 容器包括向内突出的轴向腹板,其在射弹的圆柱形部分的区域中呈现容器的内径,其对应于圆柱形部分的外径。 由腹板形成的容器的内径变得越来越大于在圆柱形部分和圆锥形部分之间的过渡区域中开始的锥形部分的相应外径,以形成延伸到容器底部的底部区域的环形间隙。 分段保持环设置在容器的内径和锥形尾部的外径之间,并且位于保持槽中并抵靠容器的内径,用于将抛射体保持在推进基座的容器中。
    • 6. 发明授权
    • Method of applying a metallic guide band to a thin-walled projectile body
    • 将金属引导带应用于薄壁射弹体的方法
    • US4797985A
    • 1989-01-17
    • US927556
    • 1986-11-06
    • Jurgen ProchnowJorg PetersUlrich TheisKlaus D. Karius
    • Jurgen ProchnowJorg PetersUlrich TheisKlaus D. Karius
    • C23C4/02C23C4/129F42B14/02B21K21/06
    • F42B14/02C23C4/02C23C4/129Y10T29/479Y10T29/49982
    • A method of applying a metallic guide band to the body of a projectile having particularly thin walls comprises making fine particles plastically deformable by heating thereof, and spraying said heated particles at high speed onto a surface section of the projectile body until a desired layer thickness of the guide band is attained. A projectile body having a circumferential guide band is produced by the method of the invention. The thin-walled projectile body has a boundary layer region on its exterior which may be roughened and/or deoxidized. The boundary layer region is formed by an intermediate layer which may be composed of molybdenum, nickel aluminide or nickel oxide and itself has a roughened boundary layer region on its exterior. This results in a particularly intimate physical bond with the particles of alloy of the guide band. The alloy is preferably of a CuZn85/15 type and has a porosity of up to 5 volume percent.
    • 将金属引导带施加到具有特别薄壁的射弹的主体的方法包括通过加热使微细颗粒塑性变形,并将所述加热的颗粒高速喷射到射弹体的表面部分上,直到所需的层厚度 引导带达到。 通过本发明的方法制造具有周向引导带的射弹体。 薄壁射弹体在其外部具有可以被粗糙化和/或脱氧的边界层区域。 边界层区域由可由钼,镍铝化物或氧化镍构成的中间层形成,其外部本身具有粗糙化的边界层区域。 这导致与引导带的合金颗粒的特别亲密的物理结合。 该合金优选为CuZn85 / 15型,并且具有高达5体积%的孔隙率。
    • 9. 发明授权
    • Subcaliber, spin stabilized multi-purpose projectile
    • Subcaliber,自旋稳定多用途射弹
    • US5872327A
    • 1999-02-16
    • US377286
    • 1989-06-23
    • Cornelis TaalBernhard BispingUlrich TheisMichaed VagedesSiegfried Kessler
    • Cornelis TaalBernhard BispingUlrich TheisMichaed VagedesSiegfried Kessler
    • F42B10/46F42B12/74F42B12/00F42B12/72
    • F42B10/46F42B12/74
    • A sub-caliber, spin stabilized multi-purpose projectile (FAPDS) made of a liquid phase sintered heavy metal sintered material composed essentially of metallic tungsten powder with additives of cobalt and nickel. To attain the highest final ballistic performance in lightly armored air and ground targets (e.g. aircraft, helicopters, armored personnel carriers) the present invention provides that the tungsten percentage of the projectile body lies between 90 and 99.5 weight percent, the density of the sintered material lies between 17.5 and 19.2 g/cm.sup.3 and the ratio of cobalt to nickel in the binder phase lies between 1:0.5 and 1:2.3, preferably 1:1.5. The projectile body according to the preferred embodiment of the invention is made of one piece and includes in its front portion a cylindrical pin for fastening of a projectile tip made of heat treatable steel. While ensuring stability during loading and firing, the projectile exhibits a highly sensitive, brittle matrix which develops in the sintered material only after the appropriate thermal treatment so that the projectile body, upon impact on the target, completely disintegrates upon encountering the slightest resistance and develops an optimum fragmentation effect.
    • 由基本上由金属钨粉末与钴和镍添加剂组成的液相烧结重金属烧结材料制成的子口径自旋稳定的多用途弹丸(FAPDS)。 为了在轻装甲空中和地面目标(例如飞机,直升机,装甲运兵车)中达到最高的最后弹道性能,本发明提出了射弹体的钨百分比在90-99.5重量%之间,烧结材料的密度 在17.5和19.2g / cm 3之间,并且粘结相中的钴与镍的比例在1:0.5至1:2.3之间,优选为1:1.5。 根据本发明的优选实施例的射弹体由一片制成,其前部包括用于固定由可热处理钢制成的射弹末端的圆柱销。 在确保装载和起火过程中的稳定性的同时,弹丸表现出一种高度敏感的脆性基体,只有经过适当的热处理才能在烧结材料中发生,从而使抛射体在受到目标影响时完全崩解, 最佳碎片效应。