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基于群体平衡的汽轮机动叶表面盐析颗粒分布特性 被引量:1
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作者 胡鹏飞 李勇 +1 位作者 曹丽华 吴雪菲 《化工进展》 EI CAS CSCD 北大核心 2018年第2期437-443,共7页
为深入了解汽轮机动叶内盐析颗粒的微观行为,本文以某超临界汽轮机高压级动叶为研究对象,应用计算流体力学与群体平衡模型耦合方法,对汽轮机动叶内盐析颗粒在流场中的分布进行数值模拟研究,获得了盐析颗粒在动叶内的粒径分布及不同负荷... 为深入了解汽轮机动叶内盐析颗粒的微观行为,本文以某超临界汽轮机高压级动叶为研究对象,应用计算流体力学与群体平衡模型耦合方法,对汽轮机动叶内盐析颗粒在流场中的分布进行数值模拟研究,获得了盐析颗粒在动叶内的粒径分布及不同负荷时叶片尾缘处盐析颗粒数量密度分布规律。模拟结果表明:在汽轮机动叶吸力面附近的盐析颗粒粒径较压力面附近盐析颗粒粒径小,且叶根处颗粒粒径小于叶顶处;动叶压力面的颗粒数量密度呈前缘点尾缘点处大、中间段小的分布规律,并且盐析颗粒在叶片上的数量密度分布最大值并不出现在组分数及粒径最大处,而是出现在平均粒径为110~150μm的盐析颗粒沉积位置处;当汽轮机30%负荷运行时,粒径40μm盐析颗粒的数量密度是其在汽轮机额定负荷运行时的1.5倍,而粒径140μm盐析颗粒的数量密度仅为汽轮机额定负荷运行时的80%。 展开更多
关键词 汽轮机动叶 盐析颗粒 群体平衡模型 两相流
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超超临界汽轮机末级动叶接触及振动特性分析 被引量:3
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作者 陈海燕 张艳春 范玮 《动力工程学报》 CAS CSCD 北大核心 2016年第3期185-190,共6页
针对超超临界汽轮机末级动叶普遍采用的凸台式阻尼拉筋、整圈自锁扭叶片结构,建立了三维非线性接触模型,采用有限元软件对某汽轮机叶片的强度及振动进行数值模拟,分析了拉筋间及围带间不同安装间隙下叶片的扭转变形,并基于设计的间隙值... 针对超超临界汽轮机末级动叶普遍采用的凸台式阻尼拉筋、整圈自锁扭叶片结构,建立了三维非线性接触模型,采用有限元软件对某汽轮机叶片的强度及振动进行数值模拟,分析了拉筋间及围带间不同安装间隙下叶片的扭转变形,并基于设计的间隙值,得到了围带及拉筋的接触状态随转速的变化规律以及非线性接触对振动特性的影响.结果表明:拉筋间及围带间的非线性接触对叶片的扭转变形和动频影响较大,可以通过调整围带、拉筋结构及其安装间隙来改变叶片的刚度和频率. 展开更多
关键词 汽轮机末级 强度振 拉筋 围带 有限元分析
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Vibrations measurements for shrouded blades of steam turbines based oneddy current sensors with high frequency response 被引量:4
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作者 YE De-chao DUAN Fa-jie +3 位作者 ZHOU Qi CHENG Zhong-hai LI Xu NIU Guang-yue 《Journal of Measurement Science and Instrumentation》 CAS CSCD 2019年第4期315-321,共7页
With the development of power plants towards high power and intelligent operation direction,the vibrations or failures of blades,especially the last stage blades in steam turbines,happen more frequently due to the uns... With the development of power plants towards high power and intelligent operation direction,the vibrations or failures of blades,especially the last stage blades in steam turbines,happen more frequently due to the unstable operating conditions brought by flexible operation.A vibration measuring method for the shrouded blades of a steam turbine based on eddy current sensors with high frequency response is proposed,meeting the requirements of non-contact heath monitoring.The eddy current sensors produce the signals which are related to the area changing of every blade’s shroud resulting from the rotation of stator.Then an improved blade tip timing(BTT)technique is proposed to detect the vibrations of shrouded blades by measuring the arrival time of each area changing signal.A structure of eddy current sensors is developed in steam turbines and an amplitude modulation/demodulation circuit is designed to improve the response bandwidth up to 250 kHz.Vibration tests for the last stage blades of a steam turbine were carried out and the results validate the efficiency of the improved BTT technique and the high frequency response of the eddy current sensors presented. 展开更多
关键词 steam turbine blade vibration measurement eddy current sensor blade tip timing
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Losses Estimation in Transonic Wet Steam Flow through Linear Blade Cascade
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作者 Sawomir Dykas Mirosaw Majkut +1 位作者 Micha Strozik Krystian Smoka 《Journal of Thermal Science》 SCIE EI CAS CSCD 2015年第2期109-116,共8页
Experimental investigations of non-equilibrium spontaneous condensation in transonic steam flow were carded out in linear blade cascade. The linear cascade consists of the stator blades of the last stage of low pressu... Experimental investigations of non-equilibrium spontaneous condensation in transonic steam flow were carded out in linear blade cascade. The linear cascade consists of the stator blades of the last stage of low pressure steam turbine. The applied experimental test section is a part of a small scale steam power plant located at Silesian Uni- versity of Technology in Gliwice. The steam parameters at the test section inlet correspond to the real conditions in low pressure part of 200MWe steam turbine. The losses in the cascade were estimated using measured static pressure and temperature behind the cascade and the total parameters at inlet. The static pressure measurements on the blade surface as well as the Schlieren pictures were used to assess the flow field in linear cascade of steam turbine stator blades. 展开更多
关键词 wet steam CONDENSATION transonic flow LOSSES
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