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Electronic/electric technology benefits studyThe benefits and payoffs of advanced electronic/electric technologies were investigated for three types of aircraft. The technologies, evaluated in each of the three airplanes, included advanced flight controls, advanced secondary power, advanced avionic complements, new cockpit displays, and advanced air traffic control techniques. For the advanced flight controls, the near term considered relaxed static stability (RSS) with mechanical backup. The far term considered an advanced fly by wire system for a longitudinally unstable airplane. In the case of the secondary power systems, trades were made in two steps: in the near term, engine bleed was eliminated; in the far term bleed air, air plus hydraulics were eliminated. Using three commercial aircraft, in the 150, 350, and 700 passenger range, the technology value and pay-offs were quantified, with emphasis on the fiscal benefits. Weight reductions deriving from fuel saving and other system improvements were identified and the weight savings were cycled for their impact on TOGW (takeoff gross weight) and upon the performance of the airframes/engines. Maintenance, reliability, and logistic support were the other criteria.
Document ID
19820020367
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Howison, W. W.
(Lockheed-California Co. Burbank, CA, United States)
Cronin, M. J.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Subject Category
Aeronautics (General)
Report/Patent Number
LR-30079
NAS 1.26:165890
NASA-CR-165890
Report Number: LR-30079
Report Number: NAS 1.26:165890
Report Number: NASA-CR-165890
Accession Number
82N28243
Funding Number(s)
CONTRACT_GRANT: NAS1-16199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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