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Rigid Body Modes These modes exist for all objects and are the modes of vibration where the object itself remains rigid and are the rotation or translational modes of the object on its mounting system. A powertrain subsystem would be expected to develop six rigid body modes on its mounts. Ideally, all six of these modes would occur below the suspension modes, below approximately 11Hz. However, the reality of vehicle and powertrain mount system design dictates that some of these modes will occur at slightly higher frequencies. Therefore, it is critical to maintain control of certain powertrain modes within this region of the frequency domain. The bounce and roll modes of a tranversely mounted, front wheel drive powertrain may couple with front suspension vertical modes (hop and tramp). Therefore, they should have separation within the frequency spectrum. It is desirable to develop a lower frequency powertrain pitch mode for optimal idle vibration isolation. The other powertrain modes may occur at higher frequencies as their respective mode shapes limit their ability to couple with suspension resonances, even if they occur at similar frequencies. A similar philosophy should be applied to other types of powertrain systems. A common way to remove the 6 rigid body modes is to fix all 6 DOF of a node. When looking for a node to fix, choose one that is not in a high stress region. If the fixed point is located in a high stress region, the optimization can be very slow. It is highly recommended that the 6 DOF of an independent node of a spider or rigid element (usually used to model joints) be selected to be fixed. On solid models, where the nodes do not have rotational stiffness; if a solid model does not have a rigid element to represent a joint, the next best way to remove the 6 rigid body modes is to fix 3 translational DOF (123) of one node, 2 translational DOF (23) of another node, and 1 translational DOF (3) of a third node. However, still make sure that the 3 nodes are not in a high stress region, otherwise this method of removing 6 rigid

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Rigid Body ModesThese modes exist for all objects and are the modes of vibration where the object itself remains rigid and are the rotation or translational modes of the object on its mounting system.

A powertrain subsystem would be expected to develop six rigid body modes on its mounts. Ideally, all six of these modes would occur below the suspension modes, below approximately 11Hz. However, the reality of vehicle and powertrain mount system design dictates that some of these modes will occur at slightly higher frequencies. Therefore, it is critical to maintain control of certain powertrain modes within this region of the frequency domain. The bounce and roll modes of a tranversely mounted, front wheel drive powertrain may couple with front suspension vertical modes (hop and tramp). Therefore, they should have separation within the frequency spectrum. It is desirable to develop a lower frequency powertrain pitch mode for optimal idle vibration isolation. The other powertrain modes may occur at higher frequencies as their respective mode shapes limit their ability to couple with suspension resonances, even if they occur at similar frequencies. A similar philosophy should be applied to other types of powertrain systems.

A common way to remove the 6 rigid body modes is to fix all 6 DOF of a node. When lookingfor a node to fix, choose one that is not in a high stress region. If the fixed point is locatedin a high stress region, the optimization can be very slow. It is highly recommended that the6 DOF of an independent node of a spider or rigid element (usually used to model joints) beselected to be fixed. On solid models, where the nodes do not have rotational stiffness; if asolid model does not have a rigid element to represent a joint, the next best way to removethe 6 rigid body modes is to fix 3 translational DOF (123) of one node, 2 translational DOF(23) of another node, and 1 translational DOF (3) of a third node. However, still make surethat the 3 nodes are not in a high stress region, otherwise this method of removing 6 rigidbody modes does not work. One way or another, all of the 6 rigid body modes of each flexiblebody must be removed. SPC, SPC1, or SPCADD (referenced in the subcase informationsection) can define the fixed DOF(pg 233 ftp://ftp.altair.com.cn/priv/support/hw12.0/hw12.0_installation/hw12_docs/OptiStruct/OptiStruct_12.0_User_Guide.pdf)

How to remove them?Constraint all dof of the rubber bearing, http://training.altairuniversity.com/wp-content/uploads/2013/08/modal_analysis_MG.pdf

Equivalent Static Load Method (ESLM)- Optimsation