DocumentCode :
157080
Title :
The effects of pole number and rotor wedge design on unbalanced magnetic pull of the synchronous generator
Author :
Petrinic, Miroslav ; Tvoric, Stjepan ; Car, Stjepan
Author_Institution :
Electr. Eng. Inst., Inc., KONCAR, Zagreb, Croatia
fYear :
2014
fDate :
2-5 Sept. 2014
Firstpage :
316
Lastpage :
322
Abstract :
In the paper, the effects of magnetic saturation and damper winding currents on the unbalanced magnetic pull of synchronous generator were analyzed by using the Finite Element Method calculations. Analyses were conducted for no load and rated load conditions on two types of generators. Firstly on the 40-pole, 10.5 MVA, salient pole synchronous generator and then on 2-pole, 40 MVA turbo generator. From the results it can be seen that magnetic saturation and damper winding currents decrease the force of unbalanced magnetic pull. In no load condition, for voltage level lower than the rated value, the maximal value of this force is achieved. In case of 2-pole generator, magnetic saturation has smaller effect on the force of unbalanced magnetic pull, than on the damper winding currents. The use of magnetic wedges on rotor can cause superposition of alternating component to the static component of the unbalanced magnetic pull.
Keywords :
magnetic fields; rotors; synchronous generators; turbogenerators; apparent power 10.5 MVA; apparent power 40 MVA; damper winding current; finite element method calculations; magnetic saturation; magnetic wedges; pole number; rotor wedge design; salient pole synchronous generator; turbo generator; unbalanced magnetic pull; Force; Generators; Magnetic flux; Magnetomechanical effects; Rotors; Saturation magnetization; Shock absorbers; electric machines; electromagnetic forces; finite element methods; generators; numerical simulation; saturation magnetization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical Machines (ICEM), 2014 International Conference on
Conference_Location :
Berlin
Type :
conf
DOI :
10.1109/ICELMACH.2014.6960199
Filename :
6960199
Link To Document :
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