纤维缠绕超高压容器承载特性研究  被引量:5

Bearing behavior of ultra-high pressure vessel with fibre winding

在线阅读下载全文

作  者:李长鹏[1] 谢淮北[1] 刘力红[1] LI Changpeng;XIE Huaibei;LIU Lihong(School of Mechanical Engineering,Anhui University of Science and Technology,Huainan 232001,China)

机构地区:[1]安徽理工大学机械工程学院,安徽淮南232001

出  处:《兵器材料科学与工程》2019年第2期25-30,共6页Ordnance Material Science and Engineering

基  金:安徽省高校自然科学重大研究项目(KJ2016SD18);安徽理工大学研究生创新基金(2017CX2031)

摘  要:为分析传统材料超高压压力容器笨重的缺陷,提出纤维缠绕超高压前混合磨料罐的设计方式。通过网格理论设计方法分析筒身段和封头段纤维铺层力学特性,计算出磨料罐筒身段及封头段缠绕纤维厚度及缠绕角。通过solidworks软件建立磨料罐三维模型,运用ANSYS软件对纤维缠绕超高压前混合磨料罐的有限元进行分析,分析其纤维铺层的主要应力、应变情况。优化磨料罐上罐口结构,并与传统结构磨料罐的结果进行对比分析。结果表明:相比于传统合金钢制成的超高压磨料罐,纤维缠绕超高压前混合磨料罐的质量减轻一半以上,提升了前混合磨料射流装置的便携性;优化上罐口结构后,纤维铺层的应力、应变数值变化更加稳定。In order to solve the heavy problem of the ultra high pressure vessel made of traditional material,and the design method of ultra-high pressure pre-mixed abrasive tank with fibre winding was proposed.Through the grid theory design method,the mechanical properties of the fiber layer in barrel section and the head section were analyzed,and the fibre-wound thickness and fibre-wound angle were calculated.The three-dimensional model of the abrasive tank was established by solid works software,and the finite element analysis was carried out by ANSYS software to analyze the main stress and strain of the fiber layer.After optimizing the structure of the upper jar of abrasive tank,ANSYS software was used to analyze and compare with the results of traditional structure.The results show that compared with the ultra high pressure abrasive tank made of the traditional alloy steel,the mass of the ultra-high pressure pre-mixed abrasive tank with fibre winding is reduced by half,which promotes the portability of pre-mixed abrasive jet device.After optimizing the structure,the changes in stress and strain of the fiber layer are more stable.

关 键 词:前混合 磨料射流 超高压 纤维缠绕 ANSYS 优化 

分 类 号:TP62[自动化与计算机技术—控制理论与控制工程]

 

参考文献:

正在载入数据...

 

二级参考文献:

正在载入数据...

 

耦合文献:

正在载入数据...

 

引证文献:

正在载入数据...

 

二级引证文献:

正在载入数据...

 

同被引文献:

正在载入数据...

 

相关期刊文献:

正在载入数据...

相关的主题
相关的作者对象
相关的机构对象