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Final report for WP4.3: Enhancement of design methods ... - Upwind

Final report for WP4.3: Enhancement of design methods ... - Upwind

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analysis. In the new multibody code, flexible components such as the blades and tower are modelled with<br />

a modal representation. However, instead <strong>of</strong> modelling the whole turbine as a single dynamic structure<br />

consisting <strong>of</strong> one rotor and tower with coupling between rotor modes and tower modes hard-wired into the<br />

code, the structure can now be modelled with any number <strong>of</strong> separate bodies, each with individual modal<br />

properties, which are coupled together using the equations <strong>of</strong> motion.<br />

Each mode is defined in terms <strong>of</strong> the following parameters:<br />

• Modal frequency<br />

• Modal damping coefficient<br />

• Mode shape represented by a vector <strong>of</strong> displacements<br />

The mode shapes and frequencies <strong>of</strong> the blade and tower (the main flexible components in a standard<br />

wind turbine model) are calculated based on the position <strong>of</strong> the neutral axis, mass distribution along the<br />

body and bending stiffness along the body, as well as other parameters specific to the body in question.<br />

The modal damping <strong>for</strong> each mode is a user input to the model.<br />

The use <strong>of</strong> multibody dynamics enables a completely self-consistent, rigorous <strong>for</strong>mulation <strong>of</strong> the structural<br />

dynamics <strong>of</strong> a wind turbine. The blade modes are modelled individually with fully coupled flapwise, edgewise<br />

and torsional degrees <strong>of</strong> freedom, and are valid <strong>for</strong> any pitch angle. Advanced definition options are<br />

available <strong>for</strong> the blade geometry and structure, and additional degrees <strong>of</strong> freedom in the drive train and<br />

gearbox can be easily modelled.<br />

For modelling the support structure a multi-member model may be used, consisting <strong>of</strong> an arbitrary spaceframe<br />

structure with any number <strong>of</strong> straight interconnecting beam elements with given mass and stiffness<br />

properties. Craig-Bampton style modes are used <strong>for</strong> the support structure, with a torsional degree <strong>of</strong> freedom<br />

included <strong>for</strong> all support structure types, not just multiple-member support structures. The support<br />

structure is not necessarily axisymmetric, so the resulting mode shapes will be three-dimensional with all<br />

six degrees <strong>of</strong> freedom at each node. Figure 2.3 shows an example <strong>of</strong> a mode shape <strong>for</strong> a braced support<br />

structure, in this case a three-legged tripod.<br />

Soil springs can be modelled in Bladed via a user-defined <strong>for</strong>ce-displacement relationship at multiple<br />

foundation stations on the sub-structure. This includes the possibility to define non-linear relationships between<br />

<strong>for</strong>ce and displacement.<br />

Figure 2.3: Example <strong>of</strong> multi-member support structure mode in Bladed<br />

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