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Structures, performance, benefit, cost studyAircraft engine structures were studied to identify the advanced structural technologies that would provide the most benefits to future aircraft operations. A series of studies identified engine systems with the greatest potential for improvements. Based on these studies, six advanced generic structural concepts were selected and conceptually designed. The benefits of each concept were quantitatively assessed in terms of thrust specific fuel consumption, weight, cost, maintenance cost, fuel burned and direct operating cost plus interest. The probability of success of each concept was also determined. The concepts were ranked and the three most promising were selected for further study which consisted of identifying and comprehensively outlining the advanced technologies required to develop these concepts for aircraft engine application. Analytic, fabrication, and test technology developments are required. The technology programs outlined emphasize the need to provide basic, fundamental understanding of technology to obtain the benefit goals.
Document ID
19810015532
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Feder, E.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-165313
PWA-5706-16
Report Number: NASA-CR-165313
Report Number: PWA-5706-16
Accession Number
81N24067
Funding Number(s)
CONTRACT_GRANT: NAS3-22050
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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