2016
DOI: 10.1002/we.2020
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Aero‐structural dynamics of a flexible hub connection for load reduction on two‐bladed wind turbines

Abstract: In this study, an innovative concept for load reduction on the two-bladed Skywind 3.4 MW prototype is presented. The load reduction system consists of a flexible coupling between the hub mount, carrying the drive train components including the hub assembly, and a nacelle carrier supported by the yaw bearing. This paper intends to assess the impact of introducing a flexible hub connection on the system dynamics and the aero-elastic response to aerodynamic load imbalances. In order to limit the rotational joint … Show more

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Cited by 10 publications
(13 citation statements)
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References 14 publications
(17 reference statements)
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“…Several studies and publications are available about the aerodynamic modeling aspects, the aero‐structural response, and the load reduction mechanisms as well as fundamental stability issues of the flexible hub connection . The dynamic response of the hub mount is influenced by the design of the interface between the hub mount and the nacelle carrier, which is assumed to act as a linear rotational spring‐damper element.…”
Section: Introductionsupporting
confidence: 77%
See 1 more Smart Citation
“…Several studies and publications are available about the aerodynamic modeling aspects, the aero‐structural response, and the load reduction mechanisms as well as fundamental stability issues of the flexible hub connection . The dynamic response of the hub mount is influenced by the design of the interface between the hub mount and the nacelle carrier, which is assumed to act as a linear rotational spring‐damper element.…”
Section: Introductionsupporting
confidence: 77%
“…The oscillation amplitude is increased for the softer configuration, and the peaks are retarded with respect to the stiffer setup. It was shown in Luhmann et al that the peak retardation along with higher oscillation amplitudes has a beneficial impact on the aerodynamic load imbalances acting on the rotor.…”
Section: Normal Operation‐hub Mount Displacementsmentioning
confidence: 99%
“…The multi-body dynamics (MBD) simulation code SIMPACK is used to simulate the structural dynamics of the turbine (as in Jassmann et al (2014) and Luhmann et al (2017)). The structural properties of the entire turbine have been modeled starting https://doi.org/10.5194/wes-2020-22 Preprint.…”
Section: Structural Modelmentioning
confidence: 99%
“…Volume sources generated by free-flow turbulence are neglected, which is justified for low Mach number flow because quadrupole volume noise is proportional to Ma 7 . This approach was validated for a rod-cylinder configuration and an airfoil in turbulent flow (Lutz et al, 2015;Illg et al, 2015). The acoustic monopole and dipole contributions to the observer sound pressure level (SPL) are computed by means of the FW-H equation.…”
Section: Acoustic Solvermentioning
confidence: 99%