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