检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
机构地区:[1]沈阳航空航天大学航空航天工程学部(院),沈阳110136
出 处:《沈阳航空航天大学学报》2015年第3期6-11,共6页Journal of Shenyang Aerospace University
摘 要:采用有限元法,建立一维和三维模型计算一个转子的临界转速,在对一维模型计算结果进行误差分析的基础上,提出一维模型的修正方法。应用此方法建立了修正极转动惯量的一维模型并计算临界转速。通过比较计算结果发现,未修正一维模型的计算结果比三维模型的高,一阶临界转速最多高96%,二阶临界转速最多高50%,采用修正极转动惯量的方法对模型进行修正后,一阶临界转速最大偏差降低至5%,二阶临界转速最大偏差降低至0.7%,计算结果接近三维模型的计算结果。By finite element method, critical speed of a rotor system is calculated using one-dimensional model and three-dimensional model respectively. Based on the error analysis of the calculation results, a cor- rection method of the one-dimensional model is proposed. This method is used to construct the one-dimen- sional model with the moment of inertia and then calculate critical speed. The comparison of the calculation results shows that the computation outcome of the one-dimensional model without correction is higher than that of the three-dimensional model. In extreme condition ,the first critical speed can be 96% higher, and the second critical speed can be 50% higher. After modifying the moment of inertia of the one-dimensional model ,the maximum deviations of the first and the second critical speeds reduce to 5% and 0. 7% respectively. The calculation results of modified one-dimensional model are close to results of the three-dimensional model.
关 键 词:转子系统 临界转速 有限元法 一维模型 模型修正
分 类 号:V211[航空宇航科学与技术—航空宇航推进理论与工程]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:3.148.182.104