建立了结构气浮静稳性分析的理论方法。导出了非对称多体气浮结构的初稳性高度的计算式。理论计算得到的稳心半径与模型试验和现场原型试验的测算值非常吻合 ;通过稳性高参数与静稳性曲线切线斜率的比较 ,气浮结构的静稳性分析理论和浮态分析理论得到了相互验证。所建立的气浮结构静稳性分析理论和浮态分析理论符合实际情况 ,可以在工程中应用 ;由于气浮力折减系数的影响 ,气浮体的浮稳性比对应的实浮体的浮稳性差 The theoretical method of structural flotation static stability analysis is established. The formula for calculating the asymptotic height of asymmetric multi-body airfoils is derived. The calculated steady-state radius is in good agreement with the calculated values ​​of the model test and the field prototype test. By comparing the slope of the tangent between the high stability parameter and the static stability curve, the static stability analysis theory and the floating state theory Mutual authentication. The established flotation stability analysis theory and floating state analysis theory are in accordance with the actual situation and can be applied in engineering. The flotation stability of the aerosol floating body is lower than that of the real floating body due to the influence of the flotation force reduction coefficient