Impact part of a projectile
    1.
    发明授权
    Impact part of a projectile 失效
    冲击弹的一部分

    公开(公告)号:US07273010B2

    公开(公告)日:2007-09-25

    申请号:US11418913

    申请日:2006-05-05

    申请人: Josef Bissig

    发明人: Josef Bissig

    IPC分类号: F42C1/00 F42B12/10

    摘要: An impact part on a projectile permits the activation of detonation systems within a large angular range of contact with a target. The impact part is provided with annular recesses with embedded circular rings that engage with the target and prevent the projectile from rebounding. A thin-walled, dome-shaped tip prevents relatively large disruptive effects upon the projectile's hollow charge. As a result of dimensioning the impact part in accordance with the rules of fracture mechanics, it is possible to achieve a desired fragmentation on the target.

    摘要翻译: 爆炸物的冲击部分允许在与目标物接触的大角度范围内激活爆轰系统。 冲击部分设置有嵌入的环形环,其与目标物接合并防止弹丸反弹。 一个薄壁的,圆顶形的尖端防止对弹丸的空心电荷产生相对较大的破坏性影响。 作为根据断裂力学规则确定冲击部件的尺寸的结果,可以在目标上实现期望的分段。

    Structure of a projectile
    2.
    发明授权

    公开(公告)号:US07273011B2

    公开(公告)日:2007-09-25

    申请号:US11432460

    申请日:2006-05-11

    申请人: Josef Bissig

    发明人: Josef Bissig

    IPC分类号: F42B12/18

    CPC分类号: F42B12/18 F42C15/00

    摘要: A projectile casing is designed to insure proper operation of the charges located therein. The charges are spaced by spacer tubes constructed such that the tubes are dispersed radially after the detonation of the preliminary charge without adversely affecting the effect of the following main charge by shock waves and/or vibrations. Solid shock barriers and damping members are provided in addition to a thin-walled projectile casing. Such a construction has proved successful, in particular, for tandem hollow charges, and also for use against active armour plating.

    Structure of a projectile
    3.
    发明申请
    Structure of a projectile 有权
    射弹的结构

    公开(公告)号:US20070051268A1

    公开(公告)日:2007-03-08

    申请号:US11432460

    申请日:2006-05-11

    申请人: Josef Bissig

    发明人: Josef Bissig

    IPC分类号: F42B12/00 F42B12/02

    CPC分类号: F42B12/18 F42C15/00

    摘要: A projectile casing is designed to insure proper operation of the charges located therein. The charges are spaced by spacer tubes constructed such that the tubes are dispersed radially after the detonation of the preliminary charge without adversely affecting the effect of the following main charge by shock waves and/or vibrations. Solid shock barriers and damping members are provided in addition to a thin-walled projectile casing. Such a construction has proved successful, in particular, for tandem hollow charges, and also for use against active armour plating.

    摘要翻译: 射弹套管设计用于确保其中的电荷的正确操作。 电荷由间隔管间隔开,隔离管被构造成使得管在预充电的引爆之后径向分散,而不会不利地影响冲击波和/或振动的下列主电荷的影响。 除了薄壁射弹套管之外,还提供了固体防震屏障和阻尼构件。 这种结构证明是成功的,特别是串联中空电荷,也用于防止主动装甲电镀。

    Impact part of a projectile
    4.
    发明申请

    公开(公告)号:US20070028792A1

    公开(公告)日:2007-02-08

    申请号:US11418913

    申请日:2006-05-05

    申请人: Josef Bissig

    发明人: Josef Bissig

    IPC分类号: F42B5/08 F42B12/00

    摘要: An impact part on a projectile permits the activation of detonation systems within a large angular range of contact with a target. The impact part is provided with annular recesses with embedded circular rings that engage with the target and prevent the projectile from rebounding. A thin-walled, dome-shaped tip prevents relatively large disruptive effects upon the projectile's hollow charge. As a result of dimensioning the impact part in accordance with the rules of fracture mechanics, it is possible to achieve a desired fragmentation on the target.

    Assembly for the optical marking of the flight path of a projectile or
aeroplane accelerated by a power unit
    5.
    发明授权
    Assembly for the optical marking of the flight path of a projectile or aeroplane accelerated by a power unit 失效
    用于由动力单元加速的射弹或飞机的飞行路径的光学标记的组装

    公开(公告)号:US5929369A

    公开(公告)日:1999-07-27

    申请号:US28702

    申请日:1998-02-24

    IPC分类号: F42B12/38 F42B12/48

    CPC分类号: F42B12/38

    摘要: An assembly for generating an optical marking of the flight path of an air/space vehicle propelled by a power unit is associated with the power unit, and mixes the marking output of the generator with either the exhaust of the power unit or air streaming past the vehicle. The generator may generate smoke or steam. In the case of a smoke generator, the assembly may include an annular chamber surrounding a central passageway through which the power unit exhaust passes. The exhaust ignites a smoke-generating charge in the annular chamber, the smoke generated passing through bores in the annular chamber.

    摘要翻译: 用于产生由动力单元推动的空气/空间车辆的飞行路径的光学标记的组件与动力单元相关联,并且将发电机的标记输出与动力单元的排气或流过空气的空气混合 车辆。 发电机可能产生烟雾或蒸气。 在烟雾发生器的情况下,组件可以包括围绕中央通道的环形室,动力单元排气穿过该环形室。 排气点燃环形室中的发烟装置,通过环形室中的孔产生的烟雾。

    Mode switching device for an electrical switch
    6.
    发明授权
    Mode switching device for an electrical switch 失效
    电开关模式开关装置

    公开(公告)号:US4843196A

    公开(公告)日:1989-06-27

    申请号:US35527

    申请日:1987-03-16

    IPC分类号: H01H3/20 H01H19/02 H01H71/74

    摘要: A mode switching or conversion device for selectively altering the operating mode of an electrical switch or other piece of equipment comprises an actuator or locking member rotatable about an axis of rotation which is disposed substantially perpendicular to the housing wall of the electrical switch. The actuator is positionally retained in an opening of this housing wall by means of a bayonet catch or joint. This actuator or locking member is provided with an axially elastic spring or resilient bracket provided with latching cams or lugs which can latch in different positions thereof into latching recesses or pockets of a latching base member of the housing.

    摘要翻译: 用于选择性地改变电开关或其他设备的操作模式的模式切换或转换装置包括围绕旋转轴线旋转的致动器或锁定构件,其基本上垂直于电气开关的壳体壁布置。 致动器通过卡口卡扣或接头位置地保持在该壳体壁的开口中。 该致动器或锁定构件设置有轴向弹性的弹簧或弹性支架,该弹簧或弹性支架设有闩锁凸轮或凸耳,其可在其不同位置处闩锁到壳体的闩锁基座部件的锁定凹部或凹穴中。