公开(公告)号：WO2006134407A1

公开(公告)日：2006-12-21

申请号：PCT/GR2006/000028

申请日：2006-06-07

Applicant: SOUKOS HIGHTECH SA ,  SOUKOS, Konstantinos

Inventor： SOUKOS, Konstantinos

IPC: F41H5/02

CPC classification number: F41H5/02 ,  F41H5/0442

Abstract: It comprises of a protective grid (12) of special configuration and hardness. In the interspaces (19) of the grid (12) there exists a polyester foam (13) for its adequate electrical insulation. The grid (12) possesses a serrate conductive entrance (14) on the side of rocket impact (40) and a conductive cathode (15) on its other side. All the electrodes (23) are connected with an electronic control unit (16) in order for the data to be transferred from the impact surfaces to this unit. The unit (16) is programmed to terminate the electric energy produced by the piezoelectric crystal to an ignition head of the Rocket Propelled Grenade RPG when this rocket strikes against the conductive entrance (14) of the protective grid (12). It can be used for the protection against the lethal Rocket propelled grenades RPG.

Abstract translation: 它由特殊构造和硬度的保护栅（12）组成。 在网格（12）的间隙（19）中，存在用于其足够的电绝缘的聚酯泡沫（13）。 格栅（12）在火箭冲击（40）的侧面上具有锯齿形导电入口（14）和在另一侧具有导电阴极（15）。 所有的电极（23）都与电子控制单元（16）连接，以使数据从冲击表面转移到该单元。 当该火箭撞击保护网格（12）的导电入口（14）时，单元（16）被编程为将由压电晶体产生的电能终止于火箭推进榴弹RPG的点火头。 它可以用于防止致命的火箭榴弹榴弹RPG。