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1.
现有文献针对计及转子变流器(RSC)控制的双馈感应风电机组(DFIG)定子短路电流解析表达,将定子磁链当作一阶直流衰减分量或忽略功率外环控制。基于DFIG电压、磁链和RSC控制方程,得到定子电流关于定子电压和定子功率的传递函数,提出定子电流的精确解析表达式。基于RSC内、外环PI参数关系,推导直流分量衰减时间常数和角频率关于PI参数的表达式。分析了RSC内外环PI参数对定子电流直流衰减分量的影响。仿真结果验证了解析表达式的准确性,为PI参数选取和保护装置测量、整定提供依据。 相似文献
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Khurram Shehzad Akhtar Ali Afzal Wardah Anam Zulfiqar Ali Tanveer Hussain 《纺织学会志》2020,111(4):555-564
AbstractIn this study, the physical–mechanical properties of ring spun, ring compact, rotor and air-vortex yarns were investigated. The study was carried with yarn having linear densities of 24.4 tex and 36.7 tex, which were then converted to woven fabrics. The ring spun yarns have higher values of strength but also with higher strength irregularities. Extra-ordinarily low hairiness was observed in air-vortex yarns due to its unique yarn formation technique. The deviation rate (DR) of yarns have correlation with the mass spectrogram of respective yarns obtained from USTER Tester 5. Rotor and air-vortex yarns exhibited higher coefficient of friction. The woven fabrics made from ring spun yarns exhibited higher tensile and tear strength with higher elongation at break. The fabrics made from air-vortex yarns have very good pilling grade due to less protruding fibres on their surface and good structural integrity. 相似文献
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为提高设计效率并快速得到适于工程应用的高压压气机转子结构,以改型设计方法为基础对某高压压气机转子结构进行了详细设计,同时对结构改进方法进行了一定的探索。采用叶—盘耦合系统循环对称结构算法及整体转子系统二维轴对称结构算法进行强度设计及改进,前轴颈最大应力下降最多达26%;其次进行支承结构设计,计算校核母型机轴承承载能力。结果表明:轴向力安全裕度最小为28%,轴承寿命大于100 000 h;给出2种调整鼠笼厚度的估算方法用以指导三维有限元计算,同时计算得到前支承刚度;通过二维有限元分析模型计算转子的临界转速,仅将后轴承支承位置沿压气机轴线向后移动7.5 mm,全运行工况转速与第2阶临界转速的安全裕度由18.5%提高到21.2%。 相似文献
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工作在高速柔轴下的柔性连接转子容易发生转子动力学失稳,柔性连接处内阻尼是引起失稳的主要因素。采用Kelvin-Voigt黏弹性理论建立转子柔性连接的复刚度内阻尼模型,通过Kelvin-Voigt黏弹性理论损耗因子与转子模态测试得到复刚度模型中代表内阻尼的虚部系数,应用拉格朗日方法建立柔性连接转子系统的动力学方程。结合试验结果验证了模型的合理性,研究了连接处内阻尼和减振器动力学参数对转子系统稳定性的影响。结果表明,增大柔性连接处内阻尼会极大降低转子系统的稳定性,增大减振器中的刚度系数和减小折合质量可有效提高稳定性,系统的稳定性需从连接处和减振器两方面协调设计。 相似文献
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Katharine Brigham Donatella Zappal Christopher J. Crabtree Christopher Donaghy‐Spargo 《风能》2020,23(4):1135-1144
This paper presents a simplified automated fault detection scheme for wind turbine induction generators with rotor electrical asymmetries. Fault indicators developed in previous works have made use of the presence of significant spectral peaks in the upper sidebands of the supply frequency harmonics; however, the specific location of these peaks may shift depending on the wind turbine speed. As wind turbines tend to operate under variable speed conditions, it may be difficult to predict where these fault‐related peaks will occur. To accommodate for variable speeds and resulting shifting frequency peak locations, previous works have introduced methods to identify or track the relevant frequencies, which necessitates an additional set of processing algorithms to locate these fault‐related peaks prior to any fault analysis. In this work, a simplified method is proposed to instead bypass the issue of variable speed (and shifting frequency peaks) by introducing a set of bandpass filters that encompass the ranges in which the peaks are expected to occur. These filters are designed to capture the fault‐related spectral information to train a classifier for automatic fault detection, regardless of the specific location of the peaks. Initial experimental results show that this approach is robust against variable speeds and further shows good generalizability in being able to detect faults at speeds and conditions that were not presented during training. After training and tuning the proposed fault detection system, the system was tested on “unseen” data and yielded a high classification accuracy of 97.4%, demonstrating the efficacy of the proposed approach. 相似文献
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从法规要求、废气初始浓度、设备、安全措施、电气控制等方面详细介绍了涂装车间采用沸石转轮浓缩吸附和氧化燃烧技术处理废气时在规划及设计过程中需注意的要点。 相似文献
10.
Georg Raimund Pirrung Maarten Paul van der Laan Nstor Ramos‐García Alexander Raul Meyer Forsting 《风能》2020,23(4):1154-1163
The loading of a wind turbine decreases towards the blade tip because of the velocities induced by the tip vortex. This tip loss effect has to be taken into account when performing actuator disc simulations, where the single blades of the turbine are not modeled. A widely used method applies a factor on the axial and tangential loading of the turbine. This factor decreases when approaching the blade tip. It has been shown that the factor should be different for the axial and tangential loading of the turbine to model the rotation of the resulting force vector at the airfoil sections caused by the induced velocity. The present article contains the derivation of a simple correction for the tangential load factor that takes this rotation into account. The correction does not need any additional curve fitting but just depends on the local airfoil characteristics and angle of attack. Actuator disc computations with the modified tip loss correction show improved agreement with results from actuator line, free wake lifting line, and blade element momentum simulations. 相似文献