EN汽轮机长叶片颤振预测方法
Flutter Prediction Method for Long Blade of Steam Turbine
- 发电技术 2021年42卷第4期 页码：500-508
- 作者机构：
哈尔滨汽轮机厂有限责任公司, 黑龙江省 哈尔滨市 150046
- 作者简介：
[ "刘长春(1976), 男, 高级工程师, 主要从事叶片结构、气动技术研究, HTCliuchangchun@163.com" ]
[ "关淳(1989), 男, 博士, 工程师, 主要从事叶片安全性评估、气动分析、叶片智能运维技术开发研究, 511298664@qq.com" ]
[ "郭魁俊(1985), 男, 硕士, 工程师, 主要从事叶片有限元强度和振动计算分析研究, 31319597@qq.com" ]
[ "李宇峰(1972), 男, 博士, 研究级高工, 主要从事叶片结构设计、强度考核、气动技术研究, liyf@harbin-electric.com" ]
[ "马义良(1983), 男, 高级工程师, 主要从事叶片机械安全性考核和评估研究, MAYL83@163.com" ]
- 基金信息：
DOI：10.12096/j.2096-4528.pgt.21001
中图分类号： TK05收稿：2021-01-19，
纸质出版：2021-08-31
- 稿件说明：
移动端阅览
刘长春, 关淳, 郭魁俊, 等. 汽轮机长叶片颤振预测方法[J]. 发电技术, 2021,42(4):500-508.
Changchun LIU, Chun GUAN, Kuijun GUO, et al. Flutter Prediction Method for Long Blade of Steam Turbine[J]. Power Generation Technology, 2021, 42(4): 500-508.
刘长春, 关淳, 郭魁俊, 等. 汽轮机长叶片颤振预测方法[J]. 发电技术, 2021,42(4):500-508. DOI： 10.12096/j.2096-4528.pgt.21001.
Changchun LIU, Chun GUAN, Kuijun GUO, et al. Flutter Prediction Method for Long Blade of Steam Turbine[J]. Power Generation Technology, 2021, 42(4): 500-508. DOI： 10.12096/j.2096-4528.pgt.21001.
摘要
基于叶片气动和结构振动仿真计算平台，建立了汽轮机长叶片流固耦合的三维计算模型。以国外某60Hz汽轮机机组次末级叶片为例，分析了叶片流场的气动特性和整圈叶片结构场的振动特性，并进一步结合能量法准则，提出了汽轮机长叶片颤振预测和评估的方法。结果表明，机组流量和叶片节径振动形式对叶片颤振特性影响很大。对于当前次末级叶片，40%流量工况时，流场内压力脉动诱导叶片颤振发生的概率为80%~90%，因此在小流量工况下需慎重使用该类叶片。基于单向流固耦合的方法，能够有效且相对快速地分析流场中脉动压力作用下的周期功，获得叶片模态振动条件下的气动阻尼系数，从而预测叶片颤振特性。
Abstract
A three-dimensional fluid-solid coupling calculation model of long blade of steam turbine was established based on the aerodynamic and structural vibration simulation platform. Taking the second last stage blade of a foreign 60Hz steam turbine unit as an example
the aerodynamic characteristics of the flow field in the single flow channel and the vibration characteristics of the entire blade structure field were analyzed. Combined with the energy method criterion
a method for predicting and evaluating the flutter of the steam turbine long blade was further proposed. The results show that the unit flow rate and the vibration form of blade pitch diameter have a great influence on the blade flutter characteristics. For the current 2nd last stage blade
the probability of blade flutter induced by pressure fluctuation in the flow field is between 80% and 90% under 40% flow condition. Therefore
this kind of blade should be carefully used under the low flow condition. Based on the unidirectional liquid-solid coupling method
the periodic work under fluctuating pressure in flow field can be analyzed effectively and relatively quickly
and the aerodynamic damping coefficient under modal vibration of blade can be obtained. Thus
the flutter characteristics of blade can be predicted.
关键词
Keywords
references
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