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提出了一种机翼结构质量分配方法 ,能根据飞机总体设计参数 ,把机翼结构质量分配到承弯结构、承剪结构、分布气动载荷所需结构、起落架安装影响结构、外挂物安装影响结构、油箱安装影响结构、前缘结构、后缘结构、襟翼结构、副翼结构、机翼机身接头及其他杂项元件结构 ,共分为 12个功能结构部分。首先建立了飞机总体设计阶段机翼结构质量分配的分析模型 ;然后根据现有飞机机翼的质量和飞机总体几何参数 ,用参数优化方法确定了该分析模型中的结构修正系数 ;从而得到一个机翼结构质量分配模型。用 8架飞机的机翼所完成的算例证明了该方法的有效性和合理性。
A method of mass allocation of wing structure is proposed. According to the overall design parameters of the aircraft, the quality of the wing structure can be distributed to the structure of bearing structure, bearing structure, distribution of aerodynamic loads, the structure of landing gear installation, and the installation of external objects The structure, the influence of tank installation, the leading edge structure, the trailing edge structure, the flap structure, the aileron structure, the wing fuselage joint and other miscellaneous component structures are divided into 12 functional structure parts. Firstly, the analysis model of wing structure mass distribution in the whole design phase of the aircraft is established. Then, the structural correction coefficient in the analysis model is determined by the parameter optimization method according to the quality of the existing aircraft wings and the overall geometric parameters of the aircraft. Wing structure mass allocation model. The example done with the wings of eight aircraft proves the validity and rationality of the method.