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全復(fù)合材料主承力梁結(jié)構(gòu)研制與分析驗(yàn)證

發(fā)布時(shí)間:2018-08-01 15:56
【摘要】:根據(jù)結(jié)構(gòu)特點(diǎn)和受力特性,研制了一種全復(fù)合材料主承力梁結(jié)構(gòu)。給出了主梁的鋪層設(shè)計(jì),詳述了其成形工藝;贛SC.Patran/Nastran建立了主梁有限元分析模型,采用線性求解器對多級(jí)載荷作用下的主梁進(jìn)行了靜強(qiáng)度分析,給出了結(jié)構(gòu)應(yīng)變與位移結(jié)果。同時(shí)設(shè)計(jì)了強(qiáng)度試驗(yàn)方案,對主梁結(jié)構(gòu)進(jìn)行了靜強(qiáng)度試驗(yàn)驗(yàn)證,采集了應(yīng)變與位移信息,確定了結(jié)構(gòu)的響應(yīng)。結(jié)果表明,全復(fù)合材料主承力梁結(jié)構(gòu)滿足強(qiáng)度設(shè)計(jì)要求,為復(fù)合材料應(yīng)用于主承力結(jié)構(gòu)提供了依據(jù)。
[Abstract]:According to the structural characteristics and mechanical characteristics, a composite main bearing beam structure was developed. The layer design of the main beam is given, and the forming process is described in detail. The finite element analysis model of the main beam is established based on MSC.Patran/Nastran. The static strength of the main beam under multistage load is analyzed by linear solver, and the results of strain and displacement are given. At the same time, the strength test scheme is designed, the static strength test of the main beam structure is carried out, the information of strain and displacement is collected, and the response of the structure is determined. The results show that the full composite main bearing beam structure meets the requirements of strength design and provides the basis for the application of composite material to the main bearing structure.
【作者單位】: 中國運(yùn)載火箭技術(shù)研究院;航天材料及工藝研究所;首都航天機(jī)械公司;
【基金】:國防基礎(chǔ)科研計(jì)劃(A0320131001)
【分類號(hào)】:TB33

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