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    Projectile with cooled nose cone
    1.
    发明授权
    Projectile with cooled nose cone 失效
    具有冷鼻锥的抛射体

    公开(公告)号：US5340058A

    公开(公告)日：1994-08-23

    申请号：US950603

    申请日：1992-09-28

    申请人： Rolf Holl ,  Rudolf Rombach ,  Karl-Heinz Roosmann

    发明人： Rolf Holl ,  Rudolf Rombach ,  Karl-Heinz Roosmann

    IPC分类号： F42B12/76 ,  F42B12/80 ,  F42B15/34 ,  B64C1/38

    CPC分类号： F42B12/80 ,  F42B12/76 ,  F42B15/34 ,  Y10T152/10756

    摘要： A projectile, particularly a kinetic energy projectile, whose nose cone is cooled due to the provision of an ablation layer and a thermal insulation layer (8, 9) on the exterior of the metal hood (4) of the projectile nose cone, and due to a highly thermally conductive medium in the spaces (5, 6) between the hood (4) and the payload (3) particularly a penetrator, of the projectile.

    摘要翻译： 射弹，特别是动能弹丸，其鼻锥由于在射弹鼻锥的金属罩（4）的外部提供消融层和绝热层（8,9）而被冷却，并且由于 到发动机罩（4）和有效载荷（3）之间的空间（5,6）中的高导热介质，特别是射弹的穿透器。

    Short-range practice projectile
    2.
    发明授权
    Short-range practice projectile 失效
    短距离练习射弹

    公开(公告)号：US4911080A

    公开(公告)日：1990-03-27

    申请号：US261517

    申请日：1988-10-03

    申请人： Jurgen Leeker ,  Rudolf Rombach

    发明人： Jurgen Leeker ,  Rudolf Rombach

    IPC分类号： F42B10/50

    CPC分类号： F42B10/50

    摘要： A practice projectile has a cylindrical casing having front and rear portions; a bottom section attached to the rear portion of the cylindrical casing; a frontal nose section including at least two subcomponents which have front and rear portions. The subcomponents can assume a closed position in which the projectile has an external configuration identical to that of a live projectile having the same caliber and an open position in which the subcomponents are in a spread-apart state at a given opening angle. The rear portion of the subcomponents is pivotally connected to the front portion of the cylindrical casing. There is further provided a device for holding the subcomponents together in the closed position prior to firing the projectile. The holding device is arranged to be overcome by centrifugal forces derived from a projectile spin subsequent to firing, to thereafter allow the subcomponents to assume the open position.

    摘要翻译： 练习弹丸具有圆柱形壳体，其具有前部和后部; 底部，其连接到所述圆筒形壳体的后部; 包括至少两个具有前部和后部的子部件的正面鼻部。 子部件可以采取关闭位置，其中抛射体具有与具有相同口径和打开位置的活射弹相同的外部构造，其中副部件在给定的开度角处处于展开状态。 副部件的后部可枢转地连接到圆筒形壳体的前部。 还提供了一种用于在击发抛射体之前将子部件保持在关闭位置的装置。 保持装置布置成通过从点火之后的射弹自旋导出的离心力来克服，之后允许子部件呈现打开位置。

    Guide assembly for a missile
    3.
    发明授权
    Guide assembly for a missile 有权
    导弹导弹组装

    公开(公告)号：US06758435B2

    公开(公告)日：2004-07-06

    申请号：US10226241

    申请日：2002-08-23

    申请人： Torsten Niemeyer ,  Manfred Dieter Schwies ,  Uwe Naderhoff ,  Thomas Heitman ,  Michael Imdahl ,  Rudolf Rombach

    发明人： Torsten Niemeyer ,  Manfred Dieter Schwies ,  Uwe Naderhoff ,  Thomas Heitman ,  Michael Imdahl ,  Rudolf Rombach

    IPC分类号： F42B1014

    CPC分类号： F42B10/14

    摘要： A missile includes a missile body and a guide assembly mounted on the missile body. The guide assembly has a plurality of pivots and a plurality of vanes mounted on respective pivots for a swinging motion between a folded position of rest and a deployed flight position. The vanes are arranged for free pivotal motion during flight in response to forces acting thereon to determine the flight position. In the folded position of each vane, its center of gravity is situated at a greater distance from the longitudinal axis of the missile body than the pivotal axis of the respective vanes. Abutments limit the flight position of the vanes to a maximum angle between the length dimension of the vanes and the longitudinal axis of the missile body. The maximum angle is greater than 90°.

    摘要翻译： 导弹包括导弹体和安装在导弹体上的引导组件。 引导组件具有多个枢轴和安装在相应枢轴上的多个叶片，用于在折叠的休息位置和展开的飞行位置之间的摆动运动。 叶片被布置成在飞行期间响应于作用在其上的力来自由枢转运动以确定飞行位置。 在每个叶片的折叠位置，其重心位于距导弹体的纵向轴线比相应叶片的枢转轴线更大的距离处。 基台将叶片的飞行位置限制在叶片的长度尺寸和导弹体的纵向轴线之间的最大角度。 最大角度大于90°。