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Development of an advanced composite aileron for the L-1011 transport aircraftSignificant improvements in structural efficiency can be achieved by the utilization of advanced composites for construction of aircraft secondary structures. Careful evaluation of alternate designs and materials for the L-1011 advanced composite inboard aileron has led to the selection of several unique material combinations and easily manufactured structural configurations. The advanced composite aileron is a direct replacement for the metal aileron with a weight savings of 23 percent. Due to the configurational simplicity of the components within the composite aileron, and because it contains 50 percent fewer parts and fasteners than the metal aileron, it is predicted that the composite aileron will be cost competitive with the metal aileron in a production environment. Structural analysis of the composite aileron, in conjunction with the design data, concept verification, and ground tests, indicates that the composite aileron design meets or exceeds structural requirements.
Document ID
19840019767
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Griffin, C. F.
(Lockheed-California Co. Burbank, CA, United States)
Dunning, E. G.
(Avco Corp.)
Date Acquired
September 4, 2013
Publication Date
February 1, 1982
Subject Category
Composite Materials
Report/Patent Number
LR-29911
NASA-CR-3517
NAS 1.26:3517
Accession Number
84N27836
Funding Number(s)
CONTRACT_GRANT: NAS1-15069
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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