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Fuse detonating system for airborne bomb - has electrically fired gas charge arming detonator hammer as bomb is released

机译:机载炸弹的保险丝引爆系统-释放炸弹时具有带电的气体充气武装雷管锤

摘要

The detonator for a bomb carried by an aircraft includes a coaxial cable providing an electric signal in order to arm the detonator as the bomb is dropped. The electrical signal ignites a gas charge when the bomb is released. The gas pushes a piston to compress a spring which acts on the detonator hammer. The hammer is immobilised by two balls engaging recesses in the side of the hammer. One of these balls may be released by removing the safety peg allowing a spring loaded piston to be withdrawn. The second ball is released on impact. An inertial mass normally holds in place a sliding piston which blocks the second ball (11). On impact, when the inertial mass moves and no longer holds this piston, a spring pushes the piston back, and the second ball is released, in turn releasing the detonator hammer.
机译:用于飞机携带的炸弹的雷管包括同轴电缆,该同轴电缆提供电信号,以便在炸弹落下时武装雷管。炸弹释放时,电信号会点燃气体。气体推动活塞压缩作用在雷管锤上的弹簧。锤子通过两个与锤子侧面的凹槽啮合的球固定。这些球之一可以通过卸下安全栓来释放,该安全栓允许将弹簧加载的活塞抽出。撞击时释放第二个球。惯性质量通常将滑动活塞保持在适当位置,该滑动活塞会阻塞第二个球(11)。撞击时,当惯性质量移动并且不再握住该活塞时,弹簧将活塞推回,第二个球被释放,进而释放雷管锤。

著录项

  • 公开/公告号FR2488394A1

    专利类型

  • 公开/公告日1982-02-12

    原文格式PDF

  • 申请/专利权人 PONT SUR SAMBRE ATEL MECA;

    申请/专利号FR19800017554

  • 发明设计人

    申请日1980-08-08

  • 分类号F42C1/04;F42B25/12;

  • 国家 FR

  • 入库时间 2022-08-22 12:28:49

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