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Development of a uninterrupted power system: ac and dc to dc converterThis program covered the design, fabrication and testing of an advanced development model uninterrupted power system. The input and output requirements imposed on the power processor were specified such that the unit is electrically interchangeable with existing power systems used by the Federal Aviation Administration in installations which have a history of failure due to electrical transient conditions. Input power is from either of two single-phase ac power sources or batteries with electronic selection and transfer between power sources. Battery reconditioning is automatic when either ac source is present. The output power is rated at 84OW; the nominal output is 24V at 35A. Within the 84OW limit, the regulated output voltage is adjustable from 22V to 30Vdc. Protection against continuous overloading or short circuit is provided. The unit is packaged in a standard 19-inch rack mount configuration with 7-inch panel height. Controls are on the front panel with power input and output through connectors on the rear surface. Cooling is by free convection from fin areas located on the side and rear panels. The packaged unit weighs 52.8 lbs., which can be reduced significantly if a three-phase ac power source is used.
Document ID
19740021300
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cronin, D. L.
(TRW Systems Group Redondo Beach, CA, United States)
Schoenfeld, A. D.
(TRW Systems Group Redondo Beach, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1973
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-CR-134497
Report Number: NASA-CR-134497
Accession Number
74N29413
Funding Number(s)
CONTRACT_GRANT: NAS3-15827
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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