1) spinning condition
旋转条件
1.
Numerical simulations of three dimensions two-phase flow field of tail-pipe SRM under spinning condition are carried out.
针对旋转条件下长尾喷管发动机的三维两相流场开展了一体化数值模拟,进行了旋转速度为0、100 r/min、300 r/min、500 r/min和1 000 r/min,颗粒直径为10μm、40μm、70μm和100μm条件下颗粒运动轨迹和聚集浓度分布影响的研究。
2) peeling condition
旋切条件
3) rotor
[英]['rəʊtə(r)] [美]['rotɚ]
旋转件
1.
In this paper,development and application of the dynamic balancing technique for the rotors of paper machine were introduced,the reasons that caused unbalance of the rotors and the results of unbalance were discussed.
介绍了目前国内外造纸机旋转件动平衡技术的发展与应用概况,对旋转件不平衡的产生原因及造成的后果作了分析;探讨了现场动平衡的方式及途径、发展趋势以及目前前沿性技术问题;提出在我国造纸行业开展现场动平衡技术研究与应用的显著效益和迫切性。
4) rotation unit
旋转组件
1.
The error of the rotation unit and the time asynchronous for the sake of GPS measure delay are analyzed.
基于采用旋转组件的SINS/GPS组合导航系统,讨论了系统中的旋转组件转速误差和GPS信号延迟带来的时间不同步问题,针对这些扰动造成的系统模型误差,提出将基于极小极大准则的H∞滤波用于组合导航系统的动基座对准。
2.
For the error of the rotation unit, a finite memory Kalman filter is applied to estimate the states during the initial alignment.
针对旋转组件的误差,在系统初始对准过程中,应用限定记忆的Kalman滤波进行状态估计,提高了对准精度。
5) rotating parts
旋转部件
1.
According to the characteristics of frequent fault and difficult diagnosis of rotating parts,selecting more interrelated vibration parameters as original character vectors,how to collect the characters from fault database and analyze rotating parts running conditions by applying fuzzy clustering way is demonstrated in this paper.
针对大型设备旋转部件故障模式复杂难以辨识的特点,选取与其运行状态密切相关的多个振动参数作为原始特征模式,阐述如何从故障信号数据库中,应用模糊聚类方法对旋转部件运行状态进行评判,挖掘出诊断的敏感特征参数。
2.
The echo signals of moving targets with rotating parts are analyzed in this paper;then according to their charac- teristics,a matching decomposition algorithm with a dictionary of two types of atoms,i.
分析了具有旋转部件的运动目标回波信号的特点,提出了以单频信号和正弦调频信号为原子的双信号集匹配分解法。
3.
Based on radar back scattering,unitary model of radar returns from aircraft rotating parts,such as the propellers of propeller-driven aircrafts and the rotors of helicopters are derived in detail,and the specifications of parameters in model are normalized.
基于雷达后向散射理论,详细推导并建立飞机旋转部件微多普勒特征的通用模型,对模型参数进行规范的定义和说明,运用相位调制分析了微多普勒特征产生的物理机理,并针对姿态角变化对微多普勒特征的影响进行仿真实验。
6) Rotating component
旋转构件
1.
Wireless sensor data acquisition system of rotating component;
旋转构件无线传感器数据采集系统
补充资料:旋转
分子式:
CAS号:
性质:将图像(或分子)绕一定轴线转动一定角度后能使图像复原的一类对称动作。旋转据以进行的轴线称作旋转轴,使图像绕轴后复原的最小转角称作基转角α。设α=2π/n,显然,旋转角为α整数倍的角度均能使图像复原,不难论证,在2π角度范围内独立、不等同旋转对称动作的种数为n。
CAS号:
性质:将图像(或分子)绕一定轴线转动一定角度后能使图像复原的一类对称动作。旋转据以进行的轴线称作旋转轴,使图像绕轴后复原的最小转角称作基转角α。设α=2π/n,显然,旋转角为α整数倍的角度均能使图像复原,不难论证,在2π角度范围内独立、不等同旋转对称动作的种数为n。
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参考词条