DocumentCode
232738
Title
The exploration of key aerodynamic parameters for an integrated design of wind turbine blades
Author
Yang Zhiqiang ; Yin MingHui ; Xia YaPing ; Zhou Lianjun ; Zou Yun
Author_Institution
Sch. of Autom., Nanjing Univ. of Sci. & Technol., Nanjing, China
fYear
2014
fDate
28-30 July 2014
Firstpage
7072
Lastpage
7076
Abstract
When selecting the structural parameters in an integrated structure and control design for wind turbines, the existing approaches were mainly depend on designers´ experience, resulting in a certain arbitrariness. The root cause was negligence of mechanism analysis to the coupling relationship between structure and control of wind turbines. Indeed, compared with those insensitive parameters, small changes in key parameters could often significantly improve the control performance. Accordingly, this paper proposed a simple and practical method of looking for key structural parameters as design variables, hoping to minimize the sacrifice of structural performance of wind turbines as well as achieving great improvement in control performance. Finally, specific to the aerodynamic parameters of wind turbine blades, by traversing the chord length and twist angle and comparing similar airfoils to find out the key parameters. The simulation results showed that airfoil was the key parameter, with its reasonable shape fine-tuning could significantly enhanced the performance of MPPT control of wind turbines.
Keywords
aerodynamics; blades; control system synthesis; machine control; wind turbines; MPPT control; aerodynamic parameters; airfoil; control design; integrated design; structural performance; wind turbine blades; Aerodynamics; Blades; Control systems; Rotors; Structural engineering; Wind energy; Wind turbines; Airfoil; Blade Aerodynamic Parameter; Integrated Design For Wind Turbines; Key structural Parameter;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6896167
Filename
6896167
Link To Document