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Numerical Study of Extra-Large Parachute’s Pre-Inflation in Finite Mass Situation

机译:有限质量情况下特大降落伞预充气的数值研究

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The extra-large parachutes were different from the common parachutes because of their size and opening process. Some undesirable inflation phenomena such as canopy winding and whipping usually appeared in their pre-inflation process. However, the mechanical mechanism of these phenomena was very difficult to be explained by experimental means. In this paper, the pre-inflation process in finite mass situation of an extra-large parachute was calculated by explicit finite elements. According to the results, the pre-inflation process can be subdivided into symmetric inflation stage, undesirable inflation stage, and stable inflation stage. The canopy winding and whipping mainly occurred in the second stage. With the continuous deceleration of parachute-payload system, the top of canopy without effective constraints would appear winding and whipping under the function of inertia force. The canopy winding and whipping increased the difficulty of canopy expanding and then caused asymmetric inflation. The above undesirable phenomena had a great influence on the deceleration effect and were easy to cause the recovery failure. The actual airdrop experiments also proved that the lack of effective constraints on the canopy top will cause undesirable inflation phenomena. The conclusions in this paper can also provide a reference for extra-large parachute design and research.
机译:特大降落伞由于其尺寸和打开过程而不同于普通降落伞。在其预充气过程中通常会出现一些不希望有的充气现象,例如树冠缠绕和鞭打。但是,这些现象的机械机理很难用实验手段来解释。本文利用显式有限元计算了超大型降落伞在有限质量情况下的预充气过程。根据结果​​,预充气过程可分为对称充气阶段,不期望的充气阶段和稳定的充气阶段。冠层缠绕和鞭打主要发生在第二阶段。随着降落伞有效载荷系统的不断减速,在没有惯性约束的情况下,树冠顶部在惯性力的作用下会出现缠绕和搅动。冠层的缠绕和鞭打增加了冠层扩张的难度,然后导致不对称膨胀。上述不良现象对减速效果影响很大,容易引起恢复失败。实际的空投实验还证明,在顶篷顶部缺乏有效约束会导致不良的充气现象。本文的结论也可为超大型降落伞的设计和研究提供参考。

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