导弹与航天运载技术
導彈與航天運載技術
도탄여항천운재기술
MISSILES AND SPACE VEHICLES
2014年
3期
74-78
,共5页
袁水林%何巍%唐霄汉%周鑫%吴义田
袁水林%何巍%唐霄漢%週鑫%吳義田
원수림%하외%당소한%주흠%오의전
运载火箭%捆绑机构%摩擦热%仿真
運載火箭%捆綁機構%摩抆熱%倣真
운재화전%곤방궤구%마찰열%방진
Launch vehicle%Strap-on mechanism%Frictional heat%Simulation
利用有限元热力耦合分析方法,通过对捆绑机构摩擦生热、热传导过程、对流过程、辐射过程分析,建立捆绑机构摩擦热分析有限元,探讨了摩擦系数对捆绑机构接触面及捆绑机构内部的温度影响情况。结果表明,在大载荷情况下,摩擦系数越大,捆绑机构接触面温度越高,温度变化越剧烈,对捆绑机构工作不利,因此需对捆绑机构采取润滑措施。
利用有限元熱力耦閤分析方法,通過對捆綁機構摩抆生熱、熱傳導過程、對流過程、輻射過程分析,建立捆綁機構摩抆熱分析有限元,探討瞭摩抆繫數對捆綁機構接觸麵及捆綁機構內部的溫度影響情況。結果錶明,在大載荷情況下,摩抆繫數越大,捆綁機構接觸麵溫度越高,溫度變化越劇烈,對捆綁機構工作不利,因此需對捆綁機構採取潤滑措施。
이용유한원열력우합분석방법,통과대곤방궤구마찰생열、열전도과정、대류과정、복사과정분석,건립곤방궤구마찰열분석유한원,탐토료마찰계수대곤방궤구접촉면급곤방궤구내부적온도영향정황。결과표명,재대재하정황하,마찰계수월대,곤방궤구접촉면온도월고,온도변화월극렬,대곤방궤구공작불리,인차수대곤방궤구채취윤활조시。
Through analyzing the frictional heat of strap-on mechanism, process of heat exchange,convection and radiation with the method of finite element thermodynamic coupling, the finite elements for the strap-on mechanism frictional heat analysis are established and the effect of the friction coefficient on the interface and interior temperature of the strap-on mechanism is discussed. The simulation results show that the strap-on mechanism does not perform well under high friction coefficient, which brings on high interface temperature and smart temperature change, so lubrication of strap-on mechanism is needed.