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Comparison of all-electric secondary power systems for civil subsonic transportsThree separate studies have shown operational, weight, and cost advantages for commercial subsonic transport aircraft using an all-electric secondary power system. The first study in 1982 showed that all-electric secondary power systems produced the second largest benefit compared to four other technology upgrades. The second study in 1985 showed a 10 percent weight and fuel savings using an all-electric high frequency (20 kHz) secondary power system. The last study in 1991 showed a 2 percent weight savings using today's technology (400 Hz) in an all-electric secondary power system. This paper will compare the 20 kHz and 400 Hz studies, analyze the 2 to 10 percent difference in weight savings and comment on the common benefits of the all-electric secondary power system.
Document ID
19930001268
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Renz, David D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:105852
NASA-TM-105852
E-7300
Report Number: NAS 1.15:105852
Report Number: NASA-TM-105852
Report Number: E-7300
Meeting Information
Meeting: Intersociety Energy Conversion Engineering Conference
Location: San Diego, CA
Country: United States
Start Date: August 3, 1992
End Date: August 7, 1992
Sponsors: ACS, AIAA, ANS, ASME, IEEE, AIChE, SAE
Accession Number
93N10456
Funding Number(s)
PROJECT: RTOP 538-01-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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