單旋翼無人直升機龍骨結(jié)構(gòu)可靠性拓撲優(yōu)化設(shè)計
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中圖分類號：TP391.99；V275.1；V214.1 文獻標志碼：B
Reliability topology optimization design for single rotor unmanned helicopter keel structure
WAN Zeguo， WANG Yufeng，WU Xiaoming （School of Aerospace Engineering，Xiamen University，Xiamen 3611O2，F(xiàn)ujian，China）
Abstract：As to the lightweighting of the keel structure of a certain type of single rotor unmanned helicopter，the variable density method is used for reliability topology optimization design. Starting from the reliability of the structure，two reliability topology optimization models，flexibility minimization model and stress minimization model，are established under volume constraints.The characteristics of the two optimization models are compared and analyzed，and a secondary design is carried out to obtain an optimized configuration of the single rotor unmanned helicopter keel structure. The analysis results show that the stress and displacement performance of the optimized configuration can meet the normal working requirements of the single rotor unmanned helicopter，and it reduces weight by 25.1% compared to the original design structure， achieving the goal of lightweight design.
Key words：keel； topology optimization；variable density method； lightweight； finite element
0引言
升機整機輕量化設(shè)計也成為重要的研究課題[1-3]龍骨是單旋翼直升機的主要受力部件，因此增強龍骨結(jié)構(gòu)的強度和剛度是可靠性拓撲優(yōu)化的首要問題[4]。（剩余4947字）