Mitigation of rotor thrust fluctuations through passive pitch

A rotor blade operating in an unsteady or a sheared stream experiences force fluctuations, which increase the structural requirements for both the blades and the rotor system as a whole. In this paper, we investigate whether force fluctuations can be passively mitigated without compromising the mean load. We consider a tidal turbine rotor in a shear current at a diameter-based Reynolds number of 2 x 10(7). The blades are rigid and can passively pitch. A mass-spring system acts on the spanwise axis of the blade governing the pitch kinematics. The effectiveness of this system is demonstrated with three methodologies: an analytical model based on blade element momentum theory and Theodorsen's theory, and two sets of Reynolds-averaged Navier-Stokes simulations performed with two independent codes. The analytical and the numerical models are validated against experiments and simulations in the literature. All methodologies predict a reduction of more than 80% of the thrust fluctuations. Furthermore, because of the more uniform thrust force exerted on the current, the wake behind a passive pitch blade does not diffuse the onset shear flow. This results in a more sheared wake and faster wake recovery. The present results demonstrate the potential benefits of passive pitch and may underpin future applications of this concept for different types of turbines and compressors, including wind turbines, propellers, helicopter rotors, etc.(C) 2022 The Author(s). Published by Elsevier Ltd.

Automated summary

This paper investigates the passive mitigation of force fluctuations in rotor blades without compromising the mean load. The effectiveness of a mass-spring system for passive pitch control is demonstrated through analytical models and numerical simulations, showing a reduction of over 80% in thrust fluctuations. Moreover, the use of passive pitch blades results in a more sheared wake and faster wake recovery, indicating the potential benefits for various types of turbines and compressors.