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Ground Simulation Test of 2D Dynamic Overload Environment of Fuze Launching

机译:引信推出2D动态超负荷环境的地面仿真试验

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摘要

The fuze launch process is subjected to backseat and spin overloads. To address this issue, a loading method of a 2D dynamic acceleration environment was developed in this study for testing fuze antioverload performance on ground. The techniques of flywheel energy storage, high-speed impact, and centrifugal rotation in the track are combined in a dynamic analysis and simulation. First, the flywheel is rotated at a constant speed by a variable-frequency motor to obtain high kinetic energy. Second, an impact hammer is instantaneously released on the specimen at a high speed, loading the backseat acceleration environment. Finally, the impact hammer is retracted, and the specimen is rotated in the track instead of spinning around its axis, thereby loading the centrifugal acceleration environment. The peak value and pulse width of the 2D overload acceleration can be adjusted by changing the speed of the flywheel and buffers in the abovementioned process. The experimental and simulation results observed that the peak value of backseat acceleration could reach 34,559 g, the pulse width was approximately 400 μs, and the peak value of the centrifugal acceleration was 1,020 g. The study results showed that the proposed approach fulfills the requirements of the 2D overload simulation test of the micro-electromechanical system (MEMS) fuze safety and arming mechanism. The proposed loading method has been successfully applied to ground simulation tests of the MEMS fuze safety and arming mechanism.
机译:引信启动过程受到后保护和旋转过载。为了解决这个问题,在本研究中开发了一种加载2D动态加速环境的加载方法,用于测试地面上的引信反载性能。轨道中飞轮储能,高速冲击和离心旋转的技术在动态分析和仿真中结合。首先,飞轮通过可变频率电动机以恒定速度旋转,以获得高动能。其次,撞击锤以高速瞬时释放在标本上,装载后部加速环境。最后,缩回撞击锤,并将样品旋转在轨道上而不是围绕其轴线旋转,从而加载离心加速环境。可以通过改变上述过程中的飞轮和缓冲器的速度来调整2D过载加速度的峰值和脉冲宽度。实验和仿真结果观察到后贮加速度的峰值可以达到34,559g,脉冲宽度约为400μs,离心加速度的峰值为1,020g。研究结果表明,该方法符合微机电系统(MEMS)引信安全机构的2D过载模拟试验的要求。所提出的加载方法已成功应用于MEMS引信安全和扶手机制的地面仿真试验。

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