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Process and assembly plans for low cost commercial fuselage structureCost and weight reduction for a composite structure is a result of selecting design concepts that can be built using efficient low cost manufacturing and assembly processes. Since design and manufacturing are inherently cost dependent, concurrent engineering in the form of a Design-Build Team (DBT) is essential for low cost designs. Detailed cost analysis from DBT designs and hardware verification must be performed to identify the cost drivers and relationships between design and manufacturing processes. Results from the global evaluation are used to quantitatively rank design, identify cost centers for higher ranking design concepts, define and prioritize a list of technical/economic issues and barriers, and identify parameters that control concept response. These results are then used for final design optimization.
Document ID
19930021676
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Willden, Kurtis
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Metschan, Stephen
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Starkey, Val
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA. Langley Research Center, First NASA Advanced Composites Technology Conference, Part 2
Subject Category
Composite Materials
Accession Number
93N30865
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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