DocumentCode :
588929
Title :
Research on 2MW Wind Turbine in the Three Conditions of Modal Analysis Based on ANSYS
Author :
Zhang Penglin ; Cao Li
Author_Institution :
Key Lab. of Nonferrous Alloys & Process., Lanzhou Univ. of Technol., Lanzhou, China
Volume :
2
fYear :
2012
fDate :
28-29 Oct. 2012
Firstpage :
386
Lastpage :
388
Abstract :
In order to prevent a phenomenon of the working wind tower turbine´s dumping and fracture, we had done the modal analysis for wind power tower in this paper. by introducing FEA(Finite Element Analysis) methods, the finite element model, simulating actual working conditions on the computer, can rationally solve the phenomenon above. and then, we had made modal research for wind tower turbine on three working conditions(V=10.6m/s, 25m/s, 75m/s). Empirical results show that wind power tower turbine can run safely on three working conditions and meet the strength and stiffness requirements of design at the same time. Through modal analysis for the 2MW 69m wind tower turbine, the modal results show that the lower modes´ frequency are dominant while the contribution of higher modes´ frequency of response is very small. In short, the 2MW 69m wind tower turbine met the designing and running requirements in this paper.
Keywords :
CAD; damping; design engineering; finite element analysis; fracture; mechanical engineering computing; mechanical strength; modal analysis; wind turbines; ANSYS software; FEA method; design requirement; dumping; finite element analysis; fracture; modal analysis; power 2 MW; response frequency; stiffness requirement; strength requirement; wind power tower turbine; Blades; Employee welfare; Finite element methods; Modal analysis; Poles and towers; Stress; Wind turbines; Displacement; Equivalent stress; FEA; Tower model; Wind turbine towers;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Intelligence and Design (ISCID), 2012 Fifth International Symposium on
Conference_Location :
Hangzhou
Print_ISBN :
978-1-4673-2646-9
Type :
conf
DOI :
10.1109/ISCID.2012.247
Filename :
6406020
Link To Document :
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