申秀丽, 齐晓东, 王荣桥, 胡殿印, 刘海. 航空发动机枞树形榫头/榫槽结构形状优化[J]. 工程力学, 2011, 28(12): 231-237.
引用本文: 申秀丽, 齐晓东, 王荣桥, 胡殿印, 刘海. 航空发动机枞树形榫头/榫槽结构形状优化[J]. 工程力学, 2011, 28(12): 231-237.
SHEN Xiu-li, QI Xiao-dong, WANG Rong-qiao, HU Dian-yin, LIU Hai. SHAPE OPTIMIZATION OF AERO ENGINE FIR-TREE TENON/MORTISE STRUCTURE[J]. Engineering Mechanics, 2011, 28(12): 231-237.
Citation: SHEN Xiu-li, QI Xiao-dong, WANG Rong-qiao, HU Dian-yin, LIU Hai. SHAPE OPTIMIZATION OF AERO ENGINE FIR-TREE TENON/MORTISE STRUCTURE[J]. Engineering Mechanics, 2011, 28(12): 231-237.

航空发动机枞树形榫头/榫槽结构形状优化

SHAPE OPTIMIZATION OF AERO ENGINE FIR-TREE TENON/MORTISE STRUCTURE

  • 摘要: 该文针对三齿枞树形榫头/榫槽结构,通过有效地解决设计变量、约束变量的选择问题,对该结构提出了详细的形状优化设计方法,对榫接结构的设计和改型有重大的工程意义。基于特征造型方法,对二维梯形榫头榫槽进行形状描述,进而建立了其参数化模型;基于梯度法进行灵敏度分析从众多特征参数中提取了设计变量;基于工程经验和应力准则提取了约束变量;最后,以最大当量应力最小为目标函数,使得梯形榫头榫槽结构最大当量应力减小了12%,并用光弹实验验证了此优化结果的可靠性。

     

    Abstract: This paper is concerned with three teeth fir-tree tenon/mortise structure, and a detailed method of shape optimal design is proposed by means of an effective solution of the design variables and constraint variables, which has evident engineering significance in designing and remodeling the tenon/mortise structure. With feature-based modeling method, geometry shape representation is undertaken for the 2D trapezoidal tenon/mortise structure, and then the parametric model is established. Sensitivity analysis is made available using the Gradient-based method which extracts design variables from a large number of parameters. Also constraint variables are obtained based on engineering experience and stressing standards. At last, as the objective function, the maximum equivalent stress of trapezoidal tenon/mortise structure decreases by 12% and is verified by photo-elastic experiment, proving the validity of the optimization results.

     

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