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Systems study for an Integrated Digital-Electric Aircraft (IDEA)The results of the Integrated Digital/Electric Aircraft (IDEA) Study are presented. Airplanes with advanced systems were, defined and evaluated, as a means of identifying potential high payoff research tasks. A baseline airplane was defined for comparison, typical of a 1990's airplane with advanced active controls, propulsion, aerodynamics, and structures technology. Trade studies led to definition of an IDEA airplane, with extensive digital systems and electric secondary power distribution. This airplane showed an improvement of 3% in fuel use and 1.8% in DOC relative to the baseline configuration. An alternate configuration, an advanced technology turboprop, was also evaluated, with greater improvement supported by digital electric systems. Recommended research programs were defined for high risk, high payoff areas appropriate for implementation under NASA leadership.
Document ID
19850007405
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tagge, G. E.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Irish, L. A.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Bailey, A. R.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
D6-52147
NASA-CR-3840
NAS 1.26:3840
Report Number: D6-52147
Report Number: NASA-CR-3840
Report Number: NAS 1.26:3840
Accession Number
85N15714
Funding Number(s)
CONTRACT_GRANT: NAS1-17528
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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