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固體火箭發(fā)動(dòng)機(jī)復(fù)合材料推力裙結(jié)構(gòu)優(yōu)化

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Composite material thrust skirt structure optimization on solid rocket motor

HAO Chenwei, LIU Jiaqiu, LI Jun,WU Weiping*, ZHANG Chen,ZHAO Hanyu(Harbin FRP Research Institute Co.,Ltd.,Harbin 150028)

Abstract:This paper optimizes the structureof composite material thrust skirt.The stress ofanewcomposite material thrust skirtunderload isanalyzedbyusingANSYSfinite element software,and then thecompositematerialthrustskirt structure isoptimizedforthreetimes.Thestaticanalysisofthecompositematerialthrustskirtafterstructuraloptimizationis carried outbyusing finiteelement software.Itisfoundthat thedeformationand stresstateofthecomposite materialthrust skirt is improvedafter structuraloptimization,whichcan providesomereferenceforthesubsequentdesignofcomposite material thrust skirt.

Keywords:composite material thrust skirt;structural optimization;finite element method

1引言

復(fù)合材料推力裙是固體火箭發(fā)動(dòng)機(jī)殼體的關(guān)鍵部件,用于實(shí)現(xiàn)殼體級(jí)間段連接或與其他部件的連接,是殼體的整體延伸[1]。(剩余4312字)

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