固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2015年
2期
261-266,272
,共7页
邢静忠%梁清波%刘成旭%杨涛
邢靜忠%樑清波%劉成旭%楊濤
형정충%량청파%류성욱%양도
环向缠绕%柔性芯模%厚壁筒%张力分析%张力设计
環嚮纏繞%柔性芯模%厚壁筒%張力分析%張力設計
배향전요%유성심모%후벽통%장력분석%장력설계
hoop winding%flexible mandrel%thick-walled cylinder%tension analysis%tension design
为实现不同梯度剩余张力的缠绕张力设计,揭示缠绕过程中的张力变化规律,提出逐层叠加法,研究可变形厚壁筒上环向缠绕张力与剩余张力之间的关系。基于不同材质的双层筒在外压作用下的变形和应力,获得剩余张力下降量与缠绕张力的积分关系,计算各层缠绕张力产生的外压引起内缠绕层环向应力的下降量。进而给出剩余张力函数,获得线性锥度缠绕、等张力缠绕和等力矩缠绕条件下的剩余张力解析公式。将缠绕张力与剩余张力的积分关系式化为微分方程,求解出缠绕后等剩余张力的缠绕张力解析公式。通过钢带缠绕容器和有芯模的纤维缠绕筒的等张力设计对比研究表明,该文解析公式给出的张力设计方案与现有文献完全吻合。文中模型从理论上很好地解决了柱形缠绕件的环向缠绕张力分析问题,适用于各向同性材料厚壁筒和纤维缠绕薄壁筒的缠绕分析和设计。
為實現不同梯度剩餘張力的纏繞張力設計,揭示纏繞過程中的張力變化規律,提齣逐層疊加法,研究可變形厚壁筒上環嚮纏繞張力與剩餘張力之間的關繫。基于不同材質的雙層筒在外壓作用下的變形和應力,穫得剩餘張力下降量與纏繞張力的積分關繫,計算各層纏繞張力產生的外壓引起內纏繞層環嚮應力的下降量。進而給齣剩餘張力函數,穫得線性錐度纏繞、等張力纏繞和等力矩纏繞條件下的剩餘張力解析公式。將纏繞張力與剩餘張力的積分關繫式化為微分方程,求解齣纏繞後等剩餘張力的纏繞張力解析公式。通過鋼帶纏繞容器和有芯模的纖維纏繞筒的等張力設計對比研究錶明,該文解析公式給齣的張力設計方案與現有文獻完全吻閤。文中模型從理論上很好地解決瞭柱形纏繞件的環嚮纏繞張力分析問題,適用于各嚮同性材料厚壁筒和纖維纏繞薄壁筒的纏繞分析和設計。
위실현불동제도잉여장력적전요장력설계,게시전요과정중적장력변화규률,제출축층첩가법,연구가변형후벽통상배향전요장력여잉여장력지간적관계。기우불동재질적쌍층통재외압작용하적변형화응력,획득잉여장력하강량여전요장력적적분관계,계산각층전요장력산생적외압인기내전요층배향응력적하강량。진이급출잉여장력함수,획득선성추도전요、등장력전요화등력구전요조건하적잉여장력해석공식。장전요장력여잉여장력적적분관계식화위미분방정,구해출전요후등잉여장력적전요장력해석공식。통과강대전요용기화유심모적섬유전요통적등장력설계대비연구표명,해문해석공식급출적장력설계방안여현유문헌완전문합。문중모형종이론상흔호지해결료주형전요건적배향전요장력분석문제,괄용우각향동성재료후벽통화섬유전요박벽통적전요분석화설계。
To realize varied grade of residual tension, and investigate the variety of residual tension in winding process, a su-perposition by layers method was suggested to research the relationship between winding tension and residual tension on a deform-able thick-walled cylinder. Based on deformation and stress response of a two-layered cylinder made of different materials, decrease of residual tension described by an integrated expression of winding tension was proposed to calculate decrease of circular stress in inner layers under pressure due to outer winding tension. Then analytical formulae of residual tension distribution formed by cone winding, isotension and equal torque tension strategy were obtained from the residual tension function, respectively. With differenti-al equation of winding tension and residual tension converted from the integration relation, an analytical formula of wind tension leading to isotension was given. Compared with an isotension strategy of a steel band winding vessel and an isotension strategy of a fiber winding thin-walled cylinder with a mandrel, the formula is quite consistent with winding tension result of thin-walled cylinder. The research shows that the model works very well for hoop winding tension analysis of cylindrical mandrel theoretically, which is capable of tension analysis of thick-walled isotropic cylinder and thin-walled fiber winding cylinder.