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本文介绍了一种改进型导弹紧固装置 ,它可以有效地防止导弹受到外部的冲击 ,并当发射导弹时 ,能使导弹迅速处于释放状态。该装置包括一对安装在导弹尾部的具有圆形横截面的突出柱体 ,一对固定在发射筒内表面的支撑架 ,其位置要使与该突出柱体对应的一对箝固凹槽处于预定的方向。其中一个箝固凹槽具有圆形横截面 ,另一个箝固凹槽为椭圆形 ,在径向方向有比突出柱体直径长的延长轴 ,而在垂直方向有与箝固凹槽相同的短轴
In this paper, an improved missile fastening device is introduced, which can effectively prevent the missile from being impacted by an external force and can promptly release the missile when the missile is launched. The device includes a pair of protruding cylinders having a circular cross section mounted on the tail of the missile and a pair of supporting brackets fixed on the inner surface of the cylinder in such a position that a pair of clamping grooves corresponding to the protruding cylinder are in Predetermined direction. One of the clamping recesses has a circular cross section and the other of the clamping recesses has an oval shape with an elongated axis longer than the diameter of the protruding post in the radial direction and the same length in the vertical direction as the clamping recess axis