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公开(公告)号:US4262598A
公开(公告)日:1981-04-21
申请号:US29189
申请日:1979-04-12
CPC分类号: F42C1/04
摘要: An impact delay fuse for a spin launched shell for delaying detonation of e explosive charge of the shell until after impact of the shell with a target. The impact delay fuse includes a hollow housing adapted to be positioned in the shell for rotation therewith in a first direction about a shell spin axis when the shell is launched, a detonation means for detonating the explosive charge of the shell, a rotatable locking member coaxially mounted within the housing for locking the detonation means in a loaded position, and a sensing and firing mechanism for controlling rotation of the locking member to move the locking member to a release position to release the detonation means to detonate the explosive charge of the shell. The sensing and firing mechanism comprises an inertia member and inertia mounting means for mounting the inertia member coaxially in the housing to rotate with the housing in the first direction when the shell is launched and to rotate the inertia member in the first direction relative to the housing when the shell impacts with the target. Inertia bias means biases the inertia member for rotation in a second direction, opposite to the first direction, relative to the housing and coupling means engage the locking member with the inertia member for rotation therewith only when the inertia member is rotated in the second direction relative to the housing. A time delay device is also provided for preventing movement of the inertia member relative to the housing for a predetermined period after launch to prevent premature detonation of the shell.
摘要翻译: 用于旋转发射的壳体的冲击延迟保险丝,用于延迟壳体的爆炸装料的爆炸直到壳体与靶材撞击之后。 撞击延迟保险丝包括适于定位在外壳中的中空壳体,用于当壳体被发射时围绕壳旋转轴在第一方向上旋转,用于引爆壳体的炸药的爆炸装置,可旋转的锁定构件同轴 安装在壳体内用于将引爆装置锁定在加载位置;以及感测和击发机构,用于控制锁定构件的旋转以将锁定构件移动到释放位置,以释放引爆装置以引爆壳体的炸药。 感测和击发机构包括惯性构件和惯性安装装置,用于当壳体被发射时将惯性构件同轴地安装在壳体中以随着壳体沿第一方向旋转并且使惯性构件相对于壳体沿第一方向旋转 当壳与目标相撞时。 惯性偏置装置相对于壳体沿与第一方向相反的第二方向偏置惯性构件以使其旋转,并且联接装置将锁定构件与惯性构件接合,以便仅当惯性构件相对于第二方向旋转时才与其一起旋转 到房屋 还提供了一种延迟装置,用于防止惯性构件相对于壳体在发射之后的预定时间段内的运动,以防止壳体过早爆炸。