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公开(公告)号：US4242960A
公开(公告)日：1981-01-06
申请号：US970182
申请日：1978-12-18
CPC分类号： F42B8/14
摘要： There is disclosed a missile which automatically disintegrates after a predetermined flight time. The missile is made up of several parts which are positively secured together by a locking means which is released at a predetermined time after the firing of the missile by the action of the air through which the missile passes during its flight. The invention may by used to advantage in both practice missiles and service missiles.
摘要翻译： 公开了一种在预定飞行时间后自动分解的导弹。 导弹由多个部件组成，这些部件通过锁定装置牢固地固定在一起，该锁定装置在导弹通过飞行中通过的空气的作用而被射击之后的预定时间被释放。 本发明可以在实践导弹和服务导弹中有利地使用。
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公开(公告)号：US4043268A
公开(公告)日：1977-08-23
申请号：US691975
申请日：1976-06-02
CPC分类号： F42B12/48
摘要： A segmented ejectable payload container is arranged to provide improved protection against axial separation of its segments during the firing operation. The container is formed as a hollow shell, with its outer jacket formed integral with a bottom end plate whose outer surface is recessed to receive an outwardly extending flange of an inner container jacket. The other end of the opposed jackets is removably closed by means of a threaded end plate. A second flange on the inner jacket is received in a corresponding recess of the second end plate when such end plate is in operative position. The interfaces between the flanges on the inner jackets and the recesses in the respective end plates are closed by means of a radially disposed seal. The depth of such recesses is chosen so that the outer surface of each end plate projects beyond the adjacent surface of the associated flange.
摘要翻译： 分段可排放的有效载荷容器被布置成在点火操作期间提供改进的防止其段的轴向分离的保护。 容器形成为中空的外壳，其外护套与底端板形成一体，其底表面凹入以容纳内容器护套的向外延伸的凸缘。 相对的夹克的另一端通过螺纹端板可拆卸地关闭。 当这种端板处于操作位置时，内护套上的第二凸缘被接收在第二端板的相应凹部中。 内套上的凸缘与相应端板中的凹槽之间的界面通过径向设置的密封封闭。 选择这样的凹部的深度，使得每个端板的外表面突出超出相关联凸缘的相邻表面。
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