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Fluid Similarity Criterions in Aircraft Landing Gear

机译:飞机起落架中的流体相似性准则

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Facing the design difficulty and risk of aircraft landing gear, the fluid similarity theory and model experiments are used to predict large prototype’s property, which provide guidance for hydraulic designation and selection to reduce risk. Firstly, the matrix method is used to establish the fluid similarity relationship between the prototype and the model’s luffing mechanism, and the above conclusions are used to design the prototype’s hydraulic system. Secondly, the luffing mechanism’s dynamical model with accumulator was established, the initial motion condition was set, and the pressure’s similarity ratio is obtained by simulation method. Finally, the dynamic model and similarity ratio about time, velocity and pressure are verified by the prototype and model’s experimental data.
机译:面对飞机起落架的设计难度和风险,流体相似性理论和模型实验被用于预测大型原型的性能,从而为液压设计和选择提供指导,以降低风险。首先,使用矩阵法建立原型与模型的变幅机构之间的流体相似关系,并将以上结论用于设计原型的液压系统。其次,建立了带有蓄能器的变幅机构动力学模型,设定了初始运动条件,并通过仿真方法获得了压力的相似率。最后,通过原型和模型的实验数据验证了动力学模型以及有关时间,速度和压力的相似率。

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