首页> 外国专利> Improvements to impact fuzes for spinning explosive projectiles, and more particularly to base-detonating fuzes of the type equipped with a mechanical auto-destruction device

Improvements to impact fuzes for spinning explosive projectiles, and more particularly to base-detonating fuzes of the type equipped with a mechanical auto-destruction device

机译:改进了用于旋转炸弹的冲击引信,特别是装备了机械自动毁灭装置的基础引信的引信

摘要

A percussion fuze device, especially culotte fuze, for a rotating explosive projectile, provided with a mechanical self-destruct device comprising a first rear-facing ramp and on which the centrifugal catches of the self-destruct device are supported while the speed of rotation of the projectile remains higher than a predetermined value below which an elastic system that controls an intermediate member carrying said centrifugal fasteners begins to predominate and generates the percussion of the fuze by an axial displacement of said intermediate member forwards, characterized by the fact that said mechanical self-destruction device also includes, on the paths to the axis that the centrifugal catches must follow in their housings to escape said first ramp, a second ramp, oriented towards the front, supported by a axially mobile and free to move back mass, relative to the organ non-intermediate which is carried by the centrifugal catches, under the action of the pressure exerted on said second ramp by said centrifugal catches during its exhaust path towards the axis, a path that is thus braked in the event of an impact due to the fact that the centrifugal catches then they must overcome, in order to escape to the first ramp, the inertia force, directed forward, of said mass. (Machine-translation by Google Translate, not legally binding)
机译:一种用于旋转炸药弹的打击乐器引信装置,特别是速动引信,其具有机械自毁装置,该机械自毁装置包括第一面向后的坡道,自毁装置的离心捕捉器被支撑在其上,而旋转速度为弹丸保持高于预定值,在该预定值以下,控制所述承载所述离心紧固件的中间构件的弹性系统开始占主导地位,并通过所述中间构件的向前轴向位移而产生引信的打击,其特征在于所述机械自-销毁装置还包括:在离心捕捉器必须遵循的轴线路径上,以使所述第一斜面逃逸,所述第二斜面朝向前方,由轴向可移动且自由向后移动的质量支撑离心捕捉器承载的非中间器官,在施加于所述器官上的压力的作用下所述离心斜面在其朝向轴线的排气路径期间由econd斜面制动,该路径因此在发生碰撞时被制动,这是因为离心斜面然后必须克服以克服惯性以便逃逸到第一斜面所述质量向前指向的力。 (通过Google翻译进行机器翻译,没有法律约束力)

著录项

  • 公开/公告号ES296154A1

    专利类型

  • 公开/公告日1964-07-01

    原文格式PDF

  • 申请/专利权人 BREVETS AERO-MECANIQUES S.A.;

    申请/专利号ES19640296154

  • 发明设计人

    申请日1964-02-06

  • 分类号F42C9/16;F42C9/18;

  • 国家 ES

  • 入库时间 2022-08-23 16:44:39

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