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ANTICRAFT MISSILE LAUNCHER

机译:反舰导弹发射器

摘要

FIELD: military equipment, antiaircraft missile weaponry. SUBSTANCE: antiaircraft missile launcher has a tripod with a vertically installed telescopic upright that carries a bed with the operator's seat installed for turning, tilting part with laying handwheels and launching tube fastening members furnished with handwheels of the missile launching control mechanical drive. The bed is made in the form of a T-shaped support with a hollow cross-piece, spring-loaded parallelogram linkages are installed on the ends of it. The tilting part bearings are secured on the upper bedplates of the linkages, and the lever springs are positioned inside the cross-piece. EFFECT: improved design. 2 cl, 4 dwg
机译:领域:军事装备,防空导弹武器。实质:防空导弹发射器具有一个三脚架,其垂直安装的伸缩式直立装置带有一个床,操作员座椅安装在该床上,用于转动,倾斜放置手轮的零件以及配有导弹发射控制机械驱动器手轮的发射管固定件。床为T形支撑形式,带有空心横档,弹簧加载的平行四边形连杆安装在床的两端。倾斜部件轴承固定在连杆的上底板上,杠杆弹簧位于横档内。效果:改进的设计。 2 cl,4 dwg

著录项

  • 公开/公告号RU2084804C1

    专利类型

  • 公开/公告日1997-07-20

    原文格式PDF

  • 申请/专利权人 KONSTRUKTORSKOE BYURO MASHINOSTROENIYA;

    申请/专利号RU19940036839

  • 发明设计人 GRECHISHCHEV YURIJ N;

    申请日1994-09-30

  • 分类号F41F3/04;

  • 国家 RU

  • 入库时间 2022-08-22 03:15:51

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