固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2015年
4期
573-579
,共7页
张军%史耀耀%康超%张晓扬
張軍%史耀耀%康超%張曉颺
장군%사요요%강초%장효양
剩余张力%芯模变形%热应力%张力分布
剩餘張力%芯模變形%熱應力%張力分佈
잉여장력%심모변형%열응력%장력분포
remaining tension%mandrel deformation%thermal stress%tension distribution
基于复合材料缠绕成型过程对工艺参数的要求,针对缠绕过程中芯模变形和加热温度对缠绕层应力分布影响等问题,建立温度和芯模变形作用下的缠绕张力设计数学模型。研究了温度引起缠绕层的应力分布解析模型,分析了缠绕内层和芯模在外层压力影响下制品的应力分布,结合3种典型的张力缠绕模型,研究了芯模内外径比以及张力锥度系数对缠绕层剩余张力的影响。提出实现缠绕制品等剩余张力下,初始缠绕张力和温度的理论关系。计算解析解与现有文献一致,文章考虑芯模变形和温度对制品应力影响,计算方法更符合实际,研究结果可用于缠绕张力设计和固化应力分析。
基于複閤材料纏繞成型過程對工藝參數的要求,針對纏繞過程中芯模變形和加熱溫度對纏繞層應力分佈影響等問題,建立溫度和芯模變形作用下的纏繞張力設計數學模型。研究瞭溫度引起纏繞層的應力分佈解析模型,分析瞭纏繞內層和芯模在外層壓力影響下製品的應力分佈,結閤3種典型的張力纏繞模型,研究瞭芯模內外徑比以及張力錐度繫數對纏繞層剩餘張力的影響。提齣實現纏繞製品等剩餘張力下,初始纏繞張力和溫度的理論關繫。計算解析解與現有文獻一緻,文章攷慮芯模變形和溫度對製品應力影響,計算方法更符閤實際,研究結果可用于纏繞張力設計和固化應力分析。
기우복합재료전요성형과정대공예삼수적요구,침대전요과정중심모변형화가열온도대전요층응력분포영향등문제,건립온도화심모변형작용하적전요장력설계수학모형。연구료온도인기전요층적응력분포해석모형,분석료전요내층화심모재외층압력영향하제품적응력분포,결합3충전형적장력전요모형,연구료심모내외경비이급장력추도계수대전요층잉여장력적영향。제출실현전요제품등잉여장력하,초시전요장력화온도적이론관계。계산해석해여현유문헌일치,문장고필심모변형화온도대제품응력영향,계산방법경부합실제,연구결과가용우전요장력설계화고화응력분석。
Based on the requirements of the process parameters in composite filament winding, aiming at the effect of mandrel deformation and heating temperature on the distribution of winding layers in winding process,the mathematical model of winding ten?sion was established.The analytical model of temperature?induced stress distribution in winding layers as well as the stress distribu?tion of inner layers and mandrel under the outer pressure was investigated.Based on three typical tension winding models,the influ?ence of the mandrel diameter ratio and taper tension coefficient on remaining tension was researched and the theoretical relationship of initial winding tension and temperature was proposed to achieve the equal remaining tension.The analytical solution was based on existing literature;while the deformation of mandrel and influence of temperature was taken into account.The results can be used for the stress analysis of curing and the design of winding tension.