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电涡流制动器在卧螺离心机差转速定值控制中的应用 被引量:6
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作者 潘芝渭 《化工机械》 CAS 1998年第6期43-45,共3页
介绍了电涡流制动器的结构和特性,以及由电涡流制动器、数字转速表、PID调节器和程控稳压稳流电源构成的卧螺离心机差转速定值控制装置。
关键词 卧螺离心机 电涡流动 差转速 分离设备
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节能型汽车底盘测功机
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作者 黄为民 《能源研究与信息》 1997年第4期40-43,共4页
本文对国内公安、交通、安全检测部门所使用的电涡流制动式汽车底盘测功机存在的问题进行了分析,提出了一种利用交流异步电机节能型的底盘测功方法。
关键词 汽车底盘测功机 涡流 汽车试验 节能
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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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Study on Blade Surface Flow around Wind Turbine by Using LDV Measurements 被引量:4
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作者 Tinnapob Phengpom Yasunari Kamada +3 位作者 Takao Maeda Junsuke Murata Shogo Nishimura Tasuku Matsuno 《Journal of Thermal Science》 SCIE EI CAS CSCD 2015年第2期131-139,共9页
This paper has attempted to study a mechanism of three-dimensional flow around a horizontal axis wind turbine(HAWT) rotor blade. An experimental study of the flow phenomenon in the vicinity of the wind turbine blade i... This paper has attempted to study a mechanism of three-dimensional flow around a horizontal axis wind turbine(HAWT) rotor blade. An experimental study of the flow phenomenon in the vicinity of the wind turbine blade is a challenging endeavor. In this research, the HAWT model with 2.4 m diameter was tested in the large wind tunnel. The flow around the rotating blade surface was measured simultaneously for three velocity components, and two probes were used for the synchronized measurement of three-dimensional flow components. The local velocity was detected for the single seeding particle measured in the point where three pairs of laser beams intersected. Blade sections of interest in this study are composed of radial positions r/R = 0.3, 0.5 and 0.7. Optimum and low tip speed ratio flow characteristics were also compared. The velocity flow vector, skin friction coefficient and bound circulation were calculated from LDV measurements, and the experimental research showed reasonably and clearly the experimental results. 展开更多
关键词 LDV measurement Sectional performance Wind turbine Boundary layer flow Span-wise flow
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Numerical Study of Combining Steady Vortex Generator Jets and Deflected Trailing Edge to Reduce the Blade Numbers of Low Pressure Turbine Stage
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作者 Li Chao YAN Peigang +2 位作者 Wang Xiangfeng HAN Wanjin WANG Qingchao 《Journal of Thermal Science》 SCIE EI CAS CSCD 2016年第6期511-517,共7页
A flow control system that combined steady Vortex Generator Jets and Deflected Trailing-edge(VGJs-DT) to decrease the low pressure turbine(LPT) blade numbers was presented.The effects of VGJs-DT on energy loss and flo... A flow control system that combined steady Vortex Generator Jets and Deflected Trailing-edge(VGJs-DT) to decrease the low pressure turbine(LPT) blade numbers was presented.The effects of VGJs-DT on energy loss and flow of low solidity low pressure turbine(LSLPT) cascades were studied.VGJs-DT was found to decrease the energy loss of LSLPT cascade and increase the flow turning angle.VGJs-DT decreased the solidity by 12.5%without a significant increase in energy loss.VGJs-DT was more effective than steady VGJs.VGJs-DT decreased the energy loss and increased the flow angle of the LSLPT cascade with steady VGJs.VGJs-DT can use 50%less mass flow than steady VGJs to inhibit the flow separation in the LSLPT cascade.The deflected trailing edge enhanced the ability of steady VGJs to resist flow separation.Overall,VGJs-DT can be used to control flow separation in LPT cascade and reduce the blade numbers of low pressure turbine stage. 展开更多
关键词 Vortex cascade turbine resist blade Turbine Numbers turbulence projection pitch
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