Described in this paper is a calculation formula for a single disk rotor system vibration response.
本文介绍了单圆盘转子体系振动响应的计算公式。
Disk rotor spider of large hydrogenerators has many advantages, such as high rigidity and benefit for ventilation.
大型水轮发电机圆盘式转子支架具有刚度大，通风好等特点。
Its disk rotor, composed solely of copper and insulator, achieves high dynamics and excellent regulation of motion at low speed, as well as silent and vibration-free functioning.
它的磁盘转子，纯粹由铜和绝缘体，达到高动力和优秀的运动速度低监管，以及沉默和震动的自由运作。
By making the infinite element model of rotor system and analyzing the dynamic characteristic on SAMCEF. Multi-disk rotor experimental rig on which auto-balancing research can be made was designed.
我们通过建立转子系统的有限元模型，利用Samcef软件对转子系统动力学特性进行分析计算，设计了多盘转子实验台来进行主动平衡研究。
This text made FEM calculation and analysis for rotor disk of heavy blower in a plant, and found that the disk can be reused safely again after the arc grooves along outside of blade being repaired.
对某发电厂大型鼓风机转子轮盘强度进行了有限元计算与分析，确认了转子轮盘在出现沿叶片外弧的弧形沟槽后，略加修复仍可安全使用。
Applying AMB to the support of HDD (hard disk drive), which can avoid the contact of bearing and HDD rotor, it has a lot of advantages in comparison with other bearing types.
将磁力轴承应用于硬盘的支承，完全消除了轴承与硬盘转子的机械接触，使硬盘具有其它轴承支承的硬盘无法企及的优点。
A new type of disk piezoelectric micromotor was given, which is non-contact between the stator and rotor.
提出了一种新型圆盘压电微电机，定子与转子间是非接触型的。
Numerical simulations and experimental investigates were carried out for unbalance response of a single disk flexible rotor system with far shaft end mounted on EORD.
通过数值仿真和实验研究远轴端eord支承的单盘柔性转子系统的不平衡响应。
Balance of the balance disk is dynamic, the pump rotor in a balanced position for the axial pulse before and after.
平衡盘的平衡状态是动态的，泵的转子在某一平衡位置会前后作轴向脉动。
The provision of a balancing member having an integral encoder disk facilitates the manufacture of the rotor assembly.
所提供的包括集成编码器圆盘的平衡元件便利于转子组件的制造。
While similar to a helicopter rotor in appearance, the autogyro's rotor must have air flowing up and through the rotor disk in order to generate rotation.
虽然与直升机外观相似，但自转旋翼机必须依靠向上流过桨叶地气流维持旋翼地旋转，产生将飞行器维持在空中地升力以及向前飞行地推力。
The simplest model of a horizontal axis wind turbine (HAWT) is one in which the turbine rotor is replaced by an actuator disk which removes energy from the wind.
水平轴风力涡轮机(HAWT)的最简单模型是：其涡轮机转子由从风力中获取能量的促动盘代替。
By combining rigid disk element and 3-d beam element the dynamical control equation of flexible rotor system and its analysis formula of coefficient matrix are developed.
将刚性圆盘单元和空间梁单元组集推导出了柔性转子系统的动力学控制方程及其系数矩阵的解析表达式。
This machine mainly by the rotor, the main axis of the plasma disk, plate device, bearing seat, drive frame, composed of large pulley.
本机主要由转子、主轴、出浆盘、筛板装置、轴承座、传动支架、大皮带轮等组成。
The nonuniform distribution of induced velocity on the rotor disk which is derived from the wang's generalized fix vortex theory is taken into account.
诱导速度在桨盘处的分布则采用王氏固定涡系涡流理论所导出的诱导速度非均布公式。
This paper introduces a comparative study of vibration characteristics of two types of rotor blades that are attached to the disk by fir-tree root and pin respectively.
本文介绍关于两种转子叶片振动特性的比较研究，这两种叶片分别是用销钉和纵树形或燕尾形榫头联接到旋转轮盘上的。
Nonlinear dynamic response of a cracked aero engine rotor with several disks is too complicated and past application oriented research in China has been limited to aero engine rotor with one disk.
研究了含有居中盘和悬臂盘的转子轴上出现裂纹时盘的非线性动态响应。
The nonuniform distribution of induced velocity on the rotor disk derived from the generalized vortex theory is taken into account.
诱导速度在桨盘处的分布采用广义涡流理论所导的公式。
The distribution of induced velocity at the rotor is assumed linearly variable over the disk.
旋翼桨盘处的诱导速度分布采用自前向后直线增大的形式。
The balancing member includes an encoder disk 42, arranged to permit the position of the rotor with respect to a stator 13 to be determined.
平衡元件包括编码器圆盘(42)，其设置用以允许测定转子相对于定子(13)的位置。
Non-linear dynamics characters of a rotor system for an elastic shaft-disk with a crack are examined by introducing the geometric non-linearity and equivalent line-spring model.
本文引入了几何非线性关系和等效线弹簧模型对含裂纹的弹性轴弹性盘转子系统进行非线性动力学分析。
Actuator disk theory yields equation (a) above for turbine maximum power, however, actuator disk theory does not yield the rotor geometry without further design theory.
促动盘理论符合上述涡轮机最大功率的方程序(a)，然而，没有进一步设计理论的情况下促动盘理论不符合转予几何学。
An experimental turbine disk was designed, and the high temperature LCF test of the rotor was carried out on the spin test rig.
设计了涡轮盘低循环疲劳试验件，在旋转试验器上进行了涡轮盘的高温低循环疲劳试验。
An experimental turbine disk was designed, and the high temperature LCF test of the rotor was carried out on the spin test rig.
设计了涡轮盘低循环疲劳试验件，在旋转试验器上进行了涡轮盘的高温低循环疲劳试验。
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