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Vibration analysis on the flexible decelerating system of terminal-sensitive submunition

机译:终端敏感子敏感系统柔性减速系统的振动分析

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The flexible decelerating parachute was predigested as a perimeter fixed roundish film in this paper. Before the rigid and flexible coupling dynamics model of the terminal-sensitive submunition was founded, the parachute had been considered as the flexible body, and the distortion of the parachute had been expressed with the hybrid coordinate method. On these basises, the floating coordinate system was founded. The parachute's distortion was divided into two parts: one was the global movement; the other was the relative distortion at the floating coordinate system. In other words, the floating coordinate system was fixed, the elastic deformation was expressed with modal spread method, and the kinematics of the terminal-sensitive submunition was analyzed. The vibration model of the flexible decelerating system was finally founded. On the base of it, the vibration analysis was simulated with ANSYS, and the natural vibration frequencies and the vibration modes of the flexible parachute system were gained. The results can provide the flexible decelerating system design of the terminal-sensitive submunition with some helpful references.
机译:在本文中,柔性减速降落伞被预先作为周边固定的圆形膜。在终端敏感子确凿的刚性和柔性耦合动力学模型成立之前,降落伞被认为是柔性的主体,并且降落伞的变形已经用混合坐标法表达。在这些基础上,建立了浮动坐标系。降落伞的扭曲分为两部分:一个是全球运动;另一个是浮动坐标系上的相对失真。换句话说,浮动坐标系是固定的,用模次涂抹方法表达弹性变形,分析了终端敏感子敏感子的运动学。终于成立了柔性减速系统的振动模型。在它的基础上,用ANSYS模拟振动分析,并且获得了自然振动频率和柔性降落伞系统的振动模式。结果可以通过一些有用的参考提供终端敏感子局的柔性减速系统设计。

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