DocumentCode :
276381
Title :
Stator core end heating in air and hydrogen indirectly cooled turbogenerators
Author :
Mecrow, B.C. ; Jack, A.G. ; Cowan, K.W.
Author_Institution :
Newcastle upon Tyne Univ., UK
fYear :
1991
fDate :
11-13 Sep 1991
Firstpage :
290
Lastpage :
294
Abstract :
Indirectly air-cooled machine and directly cooled machine end-region fields, losses and temperatures have been compared in detail. The losses in indirectly cooled machines are very substantially reduced due to a number of factors, the most dominant of which is the smaller air-gap length and lower electric loading. Other typical features, such as lower magnetic loadings and increased stator slot number also contribute to this reduction. For the two machines considered the eddy current losses in the stator core end on load are only 10% of that in the directly cooled machine. Three dimensional temperature calculations indicate that despite a poorer cooling circuit in an air-cooled machine the reduction in end-region losses is so great that only very moderate core end temperature rises occur as a result. The stator conductor bar operates at a considerably higher temperature than the core even in the end-region, and it is this feature which imposes the design limit. End-region losses are small enough to require only minimal additional design features in order to reduce them. The electric loading of air-cooled machines can be substantially increased before end-region losses become a major problem
Keywords :
cooling; eddy current losses; stators; turbogenerators; air cooling; air-gap length; directly cooled turbogenerators; eddy current losses; end-region fields; hydrogen cooling; indirectly cooled turbogenerators; losses; magnetic loadings; stator conductor bar; stator core end; stator core end heating; temperature calculations;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Electrical Machines and Drives, 1991. Fifth International Conference on (Conf. Publ. No. 341)
Conference_Location :
London
Print_ISBN :
0-85296-520-6
Type :
conf
Filename :
154011
Link To Document :
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