首页> 外国专利> STABILIZING BLOCK ADDITION TO A LAUNCH CHARGE WITH FORCEFUL UNFOLDING OF THE FINS TO BE INCLUDED IN PROJECTILES FOR USE WITH RPG-7B ROCKET PROPELLED GRENADE LAUNCHER

STABILIZING BLOCK ADDITION TO A LAUNCH CHARGE WITH FORCEFUL UNFOLDING OF THE FINS TO BE INCLUDED IN PROJECTILES FOR USE WITH RPG-7B ROCKET PROPELLED GRENADE LAUNCHER

机译:带有RPG-7B火箭推进榴弹发射器的弹药必须经过强制展开才能稳定发射的装药

摘要

The invention aims at ensuring a stable flight along the trajectory for the currently used grenade types, reducing probable deviations in their technical characteristics, increasing the distance of the direct shot and the maximum effective distance to the target, increasing the maximum range of the grenades (with or without a jet motor) with fragmentation, high-explosive, shaped charge fragmentation, thermobaric, and other action. It guarantees compatible outer ballistic characteristics for newly-developed grenade types having a higher caliber and a bigger warhead weight in comparison to the ammunition currently used for the RPG-7B. The task has been solved in way which enables a reliable function of the stabilizing block when working in an aggressive medium û momentary temperature up to 3273à3473K (3000à3200?C) and pressure of 85à90 MPa. The design presents a stabilizing block with a cross-shaped part which comprises a set-in mechanism intended for forceful unfolding of the fins of the grenade stabilizer immediately after the grenade has been propelled out of the launcher. The design allows for compensating both the lack of adequately high centrifugal forces due to turbine actionalone and the low initial velocities for grenades having a higher caliber and a bigger warhead weight which possess a high inertia moment and slow rates of rotation. The forceful unfolding of the fins immediately after the grenade has been propelled out of the launcher leads to quick fading of interfering fluctuations resulting from the stabilizer action, thus considerably reducing the flight stabilization time before the jet motor is initiated. A stable flight along the active and passive trajectory of the grenade is attained, probable deviations in grenade technical characteristics are reduced, an increase in the distance of the direct shot and the maximum effective distance to the target is achieved. An increase in the maximum range of the grenades (with or without a jet motor) with fra
机译:本发明旨在确保当前使用的手榴弹类型沿轨迹稳定飞行,减少其技术特征可能出现的偏差,增加直接射击的距离和到目标的最大有效距离,增加手榴弹的最大射程( (带有或不带有喷气发动机的情况下)具有碎裂,高爆炸性,聚能炸药碎裂,热压等作用。与目前用于RPG-7B的弹药相比,它可以保证具有更高口径和更大弹头重量的新型手榴弹的兼容外弹道特性。该任务已得到解决,当在侵蚀性介质中工作时,稳定块具有可靠的功能-瞬时温度高达3273à3473K(3000à3200?C),压力为85à90MPa。该设计方案提供了一种带有十字形部件的稳定块,该稳定块包括一个内置机构,用于在将手榴弹从发射器中推出后立即强制展开手榴弹稳定器的鳍片。这种设计既可以补偿由于单独使用涡轮机而造成的离心力不足,又可以补偿具有较高惯性矩和较慢旋转速度的,具有较高口径和较大弹头重量的榴弹的初始速度较低。在将手榴弹推出发射器后立即立即将鳍片强行展开会导致稳定器作用引起的干扰波动迅速消失,从而大大减少了启动喷气发动机之前的飞行稳定时间。实现了沿着手榴弹的主动和被动轨迹的稳定飞行,减少了手榴弹技术特性的可能偏差,增加了直接射击的距离,并且达到了到目标的最大有效距离。使用fra增加手榴弹(使用或不使用喷射马达)的最大射程

著录项

  • 公开/公告号BG110679A

    专利类型

  • 公开/公告日2011-12-30

    原文格式PDF

  • 申请/专利权人 VMZ EAD;

    申请/专利号BG20100110679

  • 申请日2010-06-16

  • 分类号F42B12/00;

  • 国家 BG

  • 入库时间 2022-08-21 17:25:32

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