共查询到20条相似文献,搜索用时 625 毫秒
1.
2.
3.
离心力作用下涡轮转子的径向变形 总被引:2,自引:0,他引:2
为了便于进一步研究叶顶间隙变化规律以及对轮盘和叶片进行强度计算,文章建立了在离心力作用下燃气轮机涡轮转子的径向变形模型。定性分析和定量计算了在不同转速和不同材料的弹性模量下,离心力对转子径向伸长量的影响。并分析了叶片离心力对轮盘变形影响的大小。所得结果表明,离心力引起的转子伸长量正比于转速的二次方;伸长量的变化率正比于转速和角加速度的乘积;且相对于叶片的径向伸长量而言,轮盘的径向变形量更为显著;叶片离心力作用在对轮盘径向变形的作用中占有一定比重;随着轮盘弹性模量增加,离心力引起的转子伸长量减小。 相似文献
4.
5.
某船用燃气轮机故障的动力学分析 总被引:2,自引:0,他引:2
针对某船用燃气轮机的压气机转子叶片与机匣碰摩故障、转子叶片叶尖磨损故障、转子轴承故障,依次分析了故障机理和振动特征,建立了燃气轮机典型故障模拟实验器,模拟了以上三种故障,采集、分析了振动信号,研制了新型的舰船旋转机械状态监测仪,为下一步的在线监测与诊断奠定了基础. 相似文献
6.
某型燃气轮机低压涡轮压气机转子动力学分析 总被引:6,自引:2,他引:4
为了获得某型燃气轮机低压涡轮压气机转子的动力学特性,并验证其稳定性及可靠性,本文使用SAMCEF/Field软件的转子动力学分析模块对该转子进行了分析计算。根据机组实际运行的条件,计算了该机组转子的临界转速、稳态不平衡响应、叶片丢失瞬态响应等。计算结果表明,临界转速安全系数合理;转子系统选取的平衡量具有较小的振动幅值;转子的瞬态响应结果验证了结构方案的合理性,转子系统具有较好的稳定性。得出了此转子结构方案能保证低压涡轮压气机稳定运行的结论。 相似文献
7.
高压涡轮叶顶间隙会直接影响到燃气轮机的功率、效率、油耗和寿命。利用有限元等软件,建立了叶片、轮盘和机匣外环的实物模型;通过热结构耦合分析,计算得到各自在温度场和离心力场作用下的径向位移,进而得到叶顶间隙变化规律,并进行了分析。计算结果表明:温度场变化是引起叶片和轮盘径向变形的主要因素;离心力对轮盘径向变形的作用比对叶片径向变形的作用要显著得多;热和离心力变化是间隙变化的两个主要因素;叶片、轮盘和机匣的热响应不一致以及离心力对转子的拉伸作用导致其径向膨胀变形不匹配,进而引起间隙变化;快速增减速度对间隙的影响最为明显。 相似文献
8.
为了分析非线性耦合因素与叶片振动对转子-轴承系统动力学特性影响,文章将叶片模化为悬臂梁结构并利用假设模态法离散简化,建立了阿尔福德(Alford)力作用下计及叶片弯曲振动的系统动力学模型。采用Runge-Kutta法对非线性振动微分方程进行数值求解,通过系统响应的分岔图、时间历程图与频谱图、轴心轨迹图、Poincaré映射图和相图研究了叶片弯曲变形以及Alford力对系统的非线性动力学行为的影响。结果表明:叶片振动使系统的不稳定区域提前,转子发生混沌运动的转速范围增大;叶尖气隙引起的Alford力使系统的运动状态变得更为复杂,油膜非线性更加明显。 相似文献
9.
为充分利用飞轮储能对船舶直流微电网功率补偿的优势,弥补燃气轮机发电系统输出功率调节响应慢的不足,对船用燃机直流微电网大功率负载下的飞轮储能系统控制策略和电网响应特性进行研究。本文基于100 kW实装微型燃气轮机发电机组,建立了包括燃气轮机、发电机、飞轮储能系统的船舶直流微电网模型,并在有无飞轮储能系统的情况下,分别突加、突卸40%、60%、80%额定功率负载,详细分析不同负载模式下直流母线电压、发电机转速和飞轮转速的变化特性。结果表明,所提出的飞轮储能系统控制策略可以及时补偿大功率负载冲击下发电机和负载之间功率不平衡,防止母线电压和同步发电机转速波动过大,有效提升微型燃气轮机发电系统的电能质量和稳定性。 相似文献
10.
11.
Several floating wind turbine designs whose hull designs reflect those used in offshore petroleum industry have emerged as leading candidates for the future development of offshore wind farms. This article presents the research findings from a model basin test program that investigated the dynamic response of a 1:50 scale model OC3 spar floating wind turbine concept designed for a water depth of 200 m. In this study the rotor was allowed to rotate freely with the wind speed and this approach eliminated some of the undesirable effects of controlling wind turbine rotational speed that were observed in earlier studies. The quality of the wind field developed by an array of fans was investigated as to its uniformity and turbulence intensity. Additional calibration tests were performed to characterize various components that included establishing the baseline wind turbine tower frequencies, stiffness of the delta type mooring system and free decay response behaviour. The assembled system was then studied under a sequence of wind and irregular wave scenarios to reveal the nature of the coupled response behaviour. The wind loads were found to have an obvious influence on the surge, heave and pitch behaviour of the spar wind turbine system. It was observed from the experimental measurements that bending moment at the top of the support tower is dominated by the 1P oscillation component and somewhat influenced by the incoming wave. Further it was determined that the axial rotor thrust and tower-top shear force have similar dynamic characteristics both dominated by tower’s first mode of vibration under wind-only condition while dominated by the incident wave field when experiencing wind-wave loading. The tensions measured in the mooring lines resulting from either wave or wind-wave excitations were influenced by the surge/pitch and heave couplings and the wind loads were found to have a clear influence on the dynamic responses of the mooring system. 相似文献
12.
13.
《船舶与海洋工程学报》2021,(2)
In this study,the coupled torsional-transverse vibration of a propeller shaft system owing to the misalignment caused by the shaft rotation was investigated.The proposed numerical model is based on the modified version of the Jeffcott rotor model.The equation of motion describing the harmonic vibrations of the system was obtained using the Euler-Lagrange equations for the associated energy functional.Experiments considering different rotation speeds and axial loads acting on the propulsion shaft system were performed to verify the numerical model.The effects of system parameters such as shaft length and diameter,stiffness and damping coefficients,and cross-section eccentricity were also studied.The cross-section eccentricity increased the displacement response,yet coupled vibrations were not initially observed.With the increase in the eccentricity,the interaction between two vibration modes became apparent,and the agreement between numerical predictions and experimental measurements improved.Given the results,the modified version of the Jeffcott rotor model can represent the coupled torsional-transverse vibration of propulsion shaft systems. 相似文献
14.
近年来,激光雷达测风已经成为一种可靠的风速测量技术,为了在风电机组控制和监测中准确高效的使用激光雷达测风数据,需要对激光雷达测风数据进行高效、快速、准确的实时处理。目前机舱式激光雷达测风面临如下问题:激光雷达在受到来流风时会跟随机舱振动,导致实测数据波动进而对风速重构算法产生影响;激光雷达会受到风电机组叶片遮挡,导致实测数据缺失或出现无效数据。本文通过合理配置激光雷达参数,以雷达测风数据作为研究对象,对测风数据进行数值修正,消除机舱振动带来的误差,开发出一套先进先出嵌套循环判断填充算法解决叶片遮挡问题,建立线性剪切风场模型,基于递推最小二乘法求解风场特征参数,最后通过泰勒冻结湍流假说计算风轮面转子有效风速,与机舱内控制参数反演出的转子有效风速进行对比,得出两组数据相关性在0.9374,两组数据差值的标准差为0.3429,结果证明在实际应用中,使用该配置参数的激光雷达通过坐标修正和数据填充等技术手段,开发的风速重构模型算法能够准确的为风电机组控制系统提供可靠的控制输入参数。 相似文献
15.
建立了某型汽轮机高压转子的完整计算模型,采用自动增量非线性通用有限元程序ADINA/ADINAT,计算在启停和变速变向过程中转子的瞬态温度场和应力场,给出了应力-时间曲线。所得结果可用于转子疲劳寿命预测。 相似文献
16.
17.
18.
19.
通过建立某型汽轮机叶片的实体模型,并基于ANSYS软件对该叶片的振动特性进行研究,利用ANSYS结构分析模块进行了模态分析,得到了叶片的前6阶固有频率和相应的振型.根据计算结果分析了汽轮机叶片的振动特性,为该叶片的设计优化和振动安全性检验提供了数值依据. 相似文献
20.
转子支承系统的刚度对其临界转速的影响 总被引:2,自引:0,他引:2
影响转子临界转速的因素很多,支承系统的刚度是其中的一个。本文采用有限元法,通过在Ansys软件中建立某微型燃气轮机支承系统的三维有限元模型,分析其静刚度和动刚度值。然后以其透平转子为例,考察支承系统的刚度值对其临界转速的影响。计算结果表明,与仅考虑轴承的刚度相比,同时考虑支承系统刚度的情况下,透平转子的临界转速下降了约40%。 相似文献