某型固体火箭发动机柔性喷管动态性能分析

L. Wenzhi, Tian Weiliang, Wu Jianxin, Liu Xiaoqin
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引用次数: 0

摘要

确定了某型号固体火箭发动机喷管的控制精度和柔性功能,针对支点中心漂移和系统的动力力矩问题,采用计算机辅助设计分析方法,建立了柔性喷管刚柔耦合多体动力学模型;以机体在系统活动中所起的供功作用对轴向载荷的阻力,对正弦波、矩形波和三角波三种激励下的动力进行了计算,得到并分析了系统的供动力矩、枢轴中心漂移、支承耳在总位移、库仑摩擦力矩、转矩和惯性力矩的偏差,同时为系统优化奠定了基础。
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Dynamic Performance Analysis of a Certain Solid Rocket Motor Flexibility Nozzle
The decision of a particular model of solid rocket motor nozzle control precision and flexible functioning of the pivot center drift and systems for power moment problems, using computer-aided design and analysis methods, and establish flexible nozzle coupled rigid-flexible multi-body dynamic model; to role of the body in the system activity for work on the axial load resistance, for sine wave, rectangular wave and triangular wave dynamics under the three kinds of incentive calculation, obtained and analyzed the system for dynamic moments, pivot center drift, supporting ear at a total displacement of, Coulomb friction torque, torque and inertia moment of deviation, while laying the foundation for the system optimization.
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