DocumentCode :
3353487
Title :
Researching on the rotor slot pitches selection rule of half-speed turbo generator based on equivalent load impedance method
Author :
Chao, Liu ; Yan-ping, Liang ; Hao, Huang ; Jun-ting, Li
Author_Institution :
Coll. of Electr. & Electron. Eng., Harbin Univ. of Sci. & Technol., Harbin, China
fYear :
2010
fDate :
26-28 June 2010
Firstpage :
4034
Lastpage :
4037
Abstract :
A method for simulating the single machine rated operating state of turbo generator by imposing equivalent load impedance on each phase winding in Ansoft external circuit is proposed. The correctness of equivalent load impedance method is proved through the comparison between calculated value and designed value of generator parameters including phase voltage, current and power factor in case of a 1,000 MW level half-speed turbo generator prototype. The synchronous reactance, voltage waveform and excitation current in the condition of different rotor slot pitches are obtained by using this method. The rotor slot pitches selection rule of half-speed turbo generator is researched through analyzing the variation regularity of synchronous reactance, voltage waveform and excitation current.
Keywords :
electric impedance; machine windings; rotors; synchronous generators; turbogenerators; Ansoft external circuit; equivalent load impedance method; excitation current; half-speed turbo generator; phase winding; power 1000 MW; rotor slot pitches; rotor slot pitches selection; single machine rated operating state; synchronous reactance; voltage waveform; Circuit simulation; Impedance measurement; Machine windings; Nuclear power generation; Power generation; Prototypes; Reactive power; Rotors; Turbogenerators; Voltage; equivalent load impedance method; half-speed turbo generator; rotor slot pitches;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechanic Automation and Control Engineering (MACE), 2010 International Conference on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-7737-1
Type :
conf
DOI :
10.1109/MACE.2010.5535893
Filename :
5535893
Link To Document :
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