NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Nuclear Brayton turboalternator-compressor (TAC) conceptual design studyA comprehensive analysis and conceptual design study of the turboalternator-compressor components was performed using HeXe as the working fluid. Individual turbine, alternator, compressor, and bearing and seal designs were evaluated. Six turboalternator-compressor TAC configurations were completed. One TAC configuration was evaluated to calculate its performance when operating under new cycle conditions,namely, one higher and one lower turbine inlet temperature and one case with krypton as the working fluid. Based on the results, a TAC configuration that incorporated a radial compressor, a radial turbine, a Lundell Alternator, and gas bearings was selected. A new layout of the TAC was prepared that reflects the cycle state points necessary to accommodate a zirconium hydride moderated reactor and a 400 Hz alternator. The final TAC design rotates at 24,000 rpm and produces 160 kWe, 480V, 3-phase, 400 hertz power.
Document ID
19720011027
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mock, E. A.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Davis, J. E.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Publication Information
Publisher: NASA
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-CR-111565
APS-5355-R
Report Number: NASA-CR-111565
Report Number: APS-5355-R
Accession Number
72N18677
Funding Number(s)
CONTRACT_GRANT: NAS3-13448
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available