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1)  component_mode synthesis method
截断模态综合法
2)  modal truncation
模态截断法
1.
For an intelligent plate with piezoceramics slices attached on both surfaces,an element model with 12 DOFs and 2 electrical DOFs is adopted and the dynamics differential equations are deduced by means of Hamilton principle,and whose order is lowered in state space by modal truncation,minimal realization and balancing xeduction.
先采用4节点矩形弯曲薄板单元(含12个位移自由度,2个电自由度)的有限元模型,利用Ham ilton原理得到了智能板结构的运动微分方程,然后综合运用模态截断法、最小实现法和平衡降阶法,对压电智能板结构的系统状态方程进行了降阶处理,得到了可观可控且低阶的近似状态方程,针对该降阶后的系统,利用H∞控制理论求解出能抑制干扰的动态输出反馈控制器,并将该控制器作用到降阶处理前的原系统中,从而能实现原系统抗干扰的振动控制。
2.
In this paper,dynamic modeling and application of the modal truncation approach(MTA) to a high-speed rotating thin elastic plate are studied.
研究了做高速旋转柔性矩形薄板的耦合动力学建模理论和模态截断法的应用。
3)  modal truncation
模态截断
1.
In order to avoid time consuming solution of equations in complex structure dynamics analysis,modal truncation method was studied herein.
以某一型号塔吊为例,验证了以DC增益作为模态截断判据的有效性,为复杂结构的动态特性分析提供了一种可行的方法。
2.
By using modal truncation technique,the frequency-domain modal transfer function and displacement response of the primary and secondary structures are obtained respectively.
建立了多点连接主次结构耦合系统的数学模型,并利用模态截断技术求出各自的模态响应传递函数和位移响应,以主次结构系统的位移功率谱密度函数在整个频率域内的积分得到位移响应的均方根值并与精确解进行比较。
3.
A mathematic model of active magnetic bearing (AMB) rotor was formulated using the modal truncation method for an experimental helium turbo rotor in a 10 MW high temperature gas cooled test module reactor.
该控制器采用模态截断的方法获得电磁轴承系统的数学模型,并采用线性二次型Gauss方法,采用了一个同LQG(linearquadraticGaussian)控制器相串联的相位补偿器,以便有效地阻尼转子的模态振动。
4)  mode truncation
模态截断
1.
Since the modes of foundation are dense,by taking the criterion of energy response as mode truncation index,the energy norm and criterion are established to calculate the mode truncated order of dynamic compaction response.
由于地基模态密集,提出以能量响应信息的收敛作为模态截断的判断指标,建立能量范数和能量判据,计算强夯动力响应的模态截断阶数。
2.
By using the modal superposition method for the dynamic responses calculation of the linear oscillation system, a judging indictor in the energy norm form is given to determine the number of dominant modes on mode truncation.
针对用模态叠加法计算结构线性振动系统的响应 ,作模态截断的截尾模态阶数的取值 ,给出了能量范数形式的判断指标 。
3.
The effect of the mode truncation on the accuracy of impact parameters identified and the dynamics of vibro impacting system is discussed through an illustrative example of two vibro impacting elastic beams.
该方法及后继的碰撞振动分析涉及到结构模态截断 。
5)  mode synthesis method
模态综合法
1.
Critical speeds of modern high-speed hollow spindle are calculated, and the influences of main structural parameters upon critical speed are also studied using component mode synthesis method.
采用子结构模态综合法计算了新型高速空心锭子的前二阶临界转速,讨论了空心锭子主要结构参数临界转速的影响,提出了适应不同工作转速的空心锭子结构参数选择范围。
2.
The bridge and the vehicle are treated as two branches of a coupling dynamic system respectively, and the mode synthesis method is applied to analyzing the responses of the coupling system.
车辆和桥梁可看成一个整体耦合动力学系统的两个分支 ,并引入模态综合法来分析其动力响应。
3.
The main problem of the mode synthesis method, applied in structural vibration analysis of prefabricated bridges, is how to select relevant number of low frequency modes synthesized during the course that displacements of substructures are expressed in generalized coordinates that are defined by displacement modes.
模态综合法应用于装配式桥梁结构振动分析的主要问题 ,是在将子结构坐标缩聚为模态广义坐标的过程中 ,如何选取适当数目的低阶模态来参与综合。
6)  component mode synthesis
模态综合法
1.
Application of component mode synthesis in ANSYS;
模态综合法在ANSYS中的应用
2.
Then,the basic principle of free interface component mode synthesis was introduced.
介绍了具有线性和非线性连接子结构的自由界面模态综合法的基本原理,并采用该方法建立了考虑副车架橡胶支承迟滞特性的整车非线性动力学模型,用所建模型对汽车动力特性进行了数值仿真,并通过试验对仿真结果进行验证。
3.
For a car including power train,engine cradle,car body,mass without spring and those substructures with linear and nonlinear joints,the scheme of component mode synthesis is employed to model dynamical systems of the car with hysteresis nonlinearity and rigid-elastic coupling.
将整车模型划分为多个子结构,包括动力总成子结构、副车架子结构、车身子结构、非簧载质量子结构及多个线性和非线性连接子结构等,采用含线性和非线性连接子结构的间接对接的自由界面模态综合法,建立整车迟滞非线性刚弹耦合系统动力学模型。
补充资料:模态综合
模态综合
component modes synthesis

   20 世纪 60 年代从航天工程中发展起来的解决复杂结构系统振动问题的有效方法。美国W.C.赫梯等人提出此法,以后被推广应用于非线性振动和随机振动响应分析。模态综合是将一个复杂结构分解成若干个较为简单的子结构。在弄清各子结构振动特性的基础上,根据对接面上的协调条件将这些子结构合成一总体结构,然后利用各子结构的振动形态得出总体结构的振动形态。用此法进行系统固有特性的求解和动力响应分析,只需计算子结构的少数几个主模态(主振型),因此能有效地缩减自由度而不改变系统的物理本质。固定界面法和自由界面法用得较为成功。此法已用于航空航天、动力、车辆、船舶和海洋工程的动力分析,效果显著。
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