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Integrated digital/electric aircraft concepts studyThe integrated digital/electrical aircraft (IDEA) is an aircraft concept which employs all electric secondary power systems and advanced digital flight control systems. After trade analysis, preferred systems were applied to the baseline configuration. An additional configuration, the alternate IDEA, was also considered. For this concept the design ground rules were relaxed in order to quantify additional synergistic benefits. It was proposed that an IDEA configuration and technical risks associated with the IDEA systems concepts be defined and the research and development required activities to reduce these risks be identified. The selected subsystems include: power generation, power distribution, actuators, environmental control system and flight controls systems. When the aircraft was resized, block fuel was predicted to decrease by 11.3 percent, with 7.9 percent decrease in direct operating cost. The alternate IDEA shows a further 3.4 percent reduction in block fuel and 3.1 percent reduction in direct operating cost.
Document ID
19850008552
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cronin, M. J.
(Lockheed-California Co. Burbank, CA, United States)
Hays, A. P.
(Lockheed-California Co. Burbank, CA, United States)
Green, F. B.
(Lockheed-California Co. Burbank, CA, United States)
Radovcich, N. A.
(Lockheed-California Co. Burbank, CA, United States)
Helsley, C. W.
(Lockheed-California Co. Burbank, CA, United States)
Rutchik, W. L.
(Lockheed-California Co. Burbank, CA, 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
NASA-CR-3841
LR-30704
NAS 1.26:3841
Accession Number
85N16861
Funding Number(s)
PROJECT: RTOP 505-45-73-01
CONTRACT_GRANT: NAS1-17529
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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