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    Device for producing missile guiding signals
    2.
    发明授权
    Device for producing missile guiding signals 失效
    用于生产导引信号的装置

    公开(公告)号：US3661346A

    公开(公告)日：1972-05-09

    申请号：US3661346D

    申请日：1969-10-10

    申请人： BOLKOW GMBH

    发明人： STANGL ARNOLD

    IPC分类号： F41G7/30 ,  F41G7/00

    CPC分类号： F41G7/303

    摘要： A device for producing signals for guiding a jet-propelled missile includes a periscope associated with an infrared goniometer, the periscope having an eyepiece and being mounted on a support plate. A hand lever is provided for manual guidance of the missile in the event that infrared guidance is ineffective and is positioned to extend in the direction of the line of sight of the periscope. This handle is positioned above the support plate of the periscope and on the side of the periscope opposite that having the eyepiece, for easy and comfortable operation by an operator.

    摘要翻译： 用于产生用于引导喷射式导弹的信号的装置包括与红外测角器相关联的潜望镜，潜望镜具有目镜并安装在支撑板上。 如果红外线引导无效且定位为在潜望镜的视线方向上延伸，则提供手柄用于导弹的手动引导。 该手柄位于潜望镜的支撑板的上方，并且与潜望镜相对的那个具有目镜的一侧，操作者容易且舒适地操作。

    Device for launching flying bodies
    3.
    发明授权
    Device for launching flying bodies 失效
    启动飞机的装置

    公开(公告)号：US3595127A

    公开(公告)日：1971-07-27

    申请号：US3595127D

    申请日：1965-07-26

    申请人： BOLKOW GMBH

    发明人： STANGL ARNOLD ,  PFISTER FRANZ

    IPC分类号： F41A1/08 ,  F41A9/45 ,  F41A23/24 ,  F41A23/34 ,  F41A23/42 ,  F41A27/06 ,  F41H7/03 ,  F41F23/00

    CPC分类号： F41A23/34 ,  F41A1/08 ,  F41A9/45 ,  F41A23/24 ,  F41A23/42 ,  F41A27/06 ,  F41H7/03

    摘要： 1. A device for launching flying bodies particularly reactiondriven missiles, comprising a substantially ball-shaped pivot member, means pivotally mounting said pivot member for pivotal movement about a first normally horizontal axis and about a second normally vertical axis, at least one first and one second flying body launching tube rotatably mounted on said pivot member, control means operatively connected to said pivotal mounting means for said pivot member for pivoting said pivot member about said first and second axes, said pivot member having a loading opening defined therethrough below the pivotal mounting of said launching tubes thereon, said first and second launching tubes being rotatable between a firing position at which one of said first and second launching tubes extends above said ball member and a loading position at which one of said first and second loading tubes extends in alignment with the loading opening defined in said ball member, and a closure flap carried by said ball member and movable between a position closing said opening and a position opening said opening.