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Load and Deformation Characteristics of Flexible Inflatable Wing Films Considering the Deformation Compensation

机译:考虑变形补偿,柔性充气翼膜的负荷和变形特性

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The flexible inflatable wings has become a hotspot with its unique advantages such as the lightweight, portability, small folding volume, fast response, low cost and so on. But because the significant geometric deformation of the flexible film appears under the inflatable pressure, which seriously affects the wing load and deformation characteristics. In this paper, considering the obvious geometrical deformation compensation influence, the pressure load, the envelope stress-strain and deformation law are studied for the flexible inflatable wing. And with the example of element of flexible wing film, the characteristics of the initial shape design and film load analysis are researched, and a analysis method of flexible deformation wing is introduced based on the deformation compensation. And the design of the flexible film load considering the deformation compensation could improve the precision of the flexible wing structure after inflating and the surface accuracy of the large deformation surface, meanwhile, the theoretical analysis method is provided for the initial design and processing of the flexible inflatable wing.
机译:柔性充气翼已成为热点,具有独特的优点,如轻质,便携性,小折叠体积,快速响应,低成本等。但是因为柔性膜的显着变形出现在充气压力下,这严重影响机翼载荷和变形特性。本文考虑了明显的几何变形补偿影响,对柔性充气翼的研究了压力负荷,包络应力 - 应变和变形法。并且随着柔性翼膜元素的例子,研究了初始形状设计和薄膜负荷分析的特性,基于变形补偿,引入了柔性变形机翼的分析方法。并且柔性薄膜负载的设计考虑变形补偿可以提高膨胀和大变形表面的表面精度的柔性翼形结构的精度,同时提供了理论分析方法,用于初始设计和加工的柔性充气翼。

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