DocumentCode :
2568746
Title :
Space Power Demonstration Engine linear alternator dynamometer test results
Author :
Dhar, M. ; Rauch, J. ; Huang, S. ; Bolton, R.
Author_Institution :
Mech. Technol. Inc., Latham, NY, USA
fYear :
1989
fDate :
6-11 Aug 1989
Firstpage :
1103
Abstract :
To verify the alternator bench test and finite element code results, it was decided to test the Space Power Demonstration Engine (SPDE) alternator on a linear dynamometer. The dynamometer tests confirmed that the primary source of losses in the SPDE alternator assembly was the adjacent magnetic structure and not the alternator proper. Alternator efficiency above 90% was demonstrated by substitution of nonmagnetic materials for the adjacent magnetic structure. A brief description is given of the SPDE alternator assembly and the MTI linear dynamometer test rig, and the dynamometer test and code prediction results are presented in detail
Keywords :
alternators; dynamometers; machine testing; space vehicle power plants; 90 percent; MTI linear dynamometer test rig; SPDE; Space Power Demonstration Engine; finite element code; linear alternator dynamometer test; nonmagnetic materials; Alternators; Assembly; Eddy currents; Finite element methods; Magnetic flux; Saturation magnetization; Space technology; Stators; Stirling engines; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
Conference_Location :
Washington, DC
Type :
conf
DOI :
10.1109/IECEC.1989.74605
Filename :
74605
Link To Document :
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