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STUDY ON THE SIMULATION TECHNIQUE OF THE VIRTUAL VIBRATION TEST FOR LIQUID ROCKET ENGINE

机译:液体火箭发动机虚拟振动试验仿真技术研究

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The simulation technique for the sinusoidal vibration test is presented. The virtual shaker system is built up firstly.The rigid-body shaker is modelled using the physical parameters of the real electrodynamic shaker. The transferfunctions of the output accelerations with the input voltages are derived using the bare shaker experiments. Theparameterized models of the shaker are obtained using the curve fitting method. Then the liquid rocket engine ismodelled with finite element method. The modal experiments for single liquid rocket engine are carried out to updatethe finite element model of the engine. Finally the virtual open-loop control sinusoidal vibration test for the engine ispresented based on the coupling of the rigid and flexible bodies. Results show that the virtual vibration test agreeswell with the experiment near the big wave crests. The virtual vibration test could reappear and the simulation resultscan also be displayed visually.
机译:提出了正弦振动试验的仿真技术。首先建立了虚拟振动筛系统。 使用实际电动振动筛的物理参数对刚体振动筛建模。转移 利用裸振动筛实验得出了输出加速度与输入电压的函数关系。这 使用曲线拟合方法获得振动筛的参数化模型。然后液体火箭发动机是 用有限元法建模。进行了单液火箭发动机的模态实验以进行更新。 发动机的有限元模型。最后,对发动机进行虚拟的开环控制正弦振动测试是 根据刚体和挠性体的耦合提出。结果表明,虚拟振动试验符合 在大波峰附近进行的实验效果很好。虚拟振动测试可能会重新出现并且模拟结果 也可以直观地显示。

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