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多支点梁结构广泛应用于客机及运输机的翼面类结构。支点的位置选择对翼面结构的变形有较大影响。本文以某型飞机襟翼为例,研究了适用于翼面类结构支撑位置选择的计算过程,为翼面结构后续刚度设计与变形控制提供基础。
Multi-fulcrum beam structure is widely used in passenger aircraft and transport aircraft wing type structure. The location of the fulcrum has a greater impact on the deformation of the airfoil. Taking a certain type of aircraft flap as an example, this paper studies the calculation process for the choice of support position of airfoil structure, and provides the basis for the subsequent stiffness design and deformation control of the airfoil structure.