| 基于升速响应信息柔性转子系统的多阶多平面瞬态动平衡方法 |
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| 引用本文： | 岳聪,任兴民,邓旺群,杨永锋.基于升速响应信息柔性转子系统的多阶多平面瞬态动平衡方法[J].航空动力学报,2013,28(11):2593-2599. |
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| 作者姓名： | 岳聪 任兴民 邓旺群 杨永锋 |
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| 作者单位： | 西北工业大学 力学与土木建筑学院 振动工程研究所, 西安 710007;西北工业大学 力学与土木建筑学院 振动工程研究所, 西安 710007;中国航空工业集团公司 中国航空动力机械研究所, 湖南 株洲 412002;西北工业大学 力学与土木建筑学院 振动工程研究所, 西安 710007 |
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| 基金项目： | 国家自然科学基金(11272257);航空科学基金(20112108001);陕西省自然科学基础研究计划(JC201242) |
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| 摘 要： | 利用升速响应信息进行柔性转子多阶、多平面瞬态动平衡方法研究.在提出柔性转子越过各阶临界转速时平衡校正量最优值算法的基础上,建立了以3次起车即可实现同时抑制多阶不平衡达到整体平衡的方法.通过所提出的平衡方法分别对双盘转子模型前2阶不平衡和三盘转子模型前3阶不平衡进行动平衡仿真研究,结果显示:该方法能在整体上有效控制转子系统的振幅波动,越过临界转速时的振幅减幅率普遍在80%左右,最低可达到60%以上.
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| 关 键 词： | 升速响应 柔性转子 模态平衡 加速过程 不平衡识别 |
| 收稿时间： | 2012/10/11 0:00:00 |
Multi-plane and multi-critical transient dynamic balance method based on rising speed response information of flexible rotor system |
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| YUE Cong,REN Xing-min,DENG Wang-qun and YANG Yong-feng.Multi-plane and multi-critical transient dynamic balance method based on rising speed response information of flexible rotor system[J].Journal of Aerospace Power,2013,28(11):2593-2599. |
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| Authors: | YUE Cong REN Xing-min DENG Wang-qun and YANG Yong-feng |
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| Institution: | Institute of Vibration Engineering, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710007;Institute of Vibration Engineering, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710007;China Aviation Dynamical Machinery Research Institute, Aviation Industry Corporation of China, Zhuzhou Hunan 412002, China;Institute of Vibration Engineering, School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710007 |
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| Abstract: | A multi-plane and multi-critical transient dynamic balance method was proposed by rising speed response information of flexible rotor.The flexible rotor multi-critical speed balance correction quantity under the optimal algorithm was put forward.The overall balance can be realized by imbalance information of three times rise-critical-speed re-sponse to suppress multi-critical amount of unbalance simultaneously. Numerical simulation with dynamic balance method applies to two-disk rotor model of two-critical unbalance and three-disk rotor model of three-critical unbalance, respectively. The results show that the method could effectively control the amplitude fluc-tuation of whole rotor system while decreasing critical speed amplitude rate up to 60%-80%. |
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| Keywords: | rising speed response flexible rotor modal balancing accelerate process unbalance identification |
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