Design, Optimization and Manufacturing of Metallic Wings of Light Aircraft

Aerotecnica Missili & Spazio

View Publication Info
 
 
Field Value
 
Title Design, Optimization and Manufacturing of Metallic Wings of Light Aircraft
 
Creator Cipolla, Vittorio
Binante, Vincenzo
Nardone, Angelo
 
Subject Structures, Aircraft Design
Welding, Wing structures, Optimization
FEM, Structural Optimization, Technologies
 
Description Most of the wing structures of modern leisure and sport aircraft, such as LSA, VLA, ultralights, etc., are made of composite materials.These latter allow for high surface quality and lower costs, if compared to metallic solutions with conventional riveted technology, which would be adopted as production volumes are small. Assuming a greater production volume, proper of an industrial production, the metallic solution can become a viable alternative considering an automatic welding technology, instead of riveted junctions. Although welded solutions bring with them issues in terms of fatigue resistance, the low wing loading typical of LSA/VLA allows to mitigate the mass increase and to obtain a proper design. This paper shows how wing structures made of light metallic alloys with welded junctions could be a feasible solution, presenting some results related to the design of an innovative light amphibian object of study within the research project "IDINTOS".The activities here presented concern the optimization methodology for the design of metallic wing structures, the detail design through Finite Element Methods and the set-up of a technology demonstrator of the manufacturing process.
 
Publisher Associazione Italiana di Aeronautica e Astronautica (AIDAA)
 
Contributor
 
Date 2019-01-24
 
Type info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
Peer-reviewed Article
Numerical, Experimental
 
Format application/pdf
 
Identifier http://131.114.27.37/index.php/AMS/article/view/350
10.19249/ams.v97i4.350
 
Source Aerotecnica Missili & Spazio; Vol 97, No 4 (2018); 219-227
0365-7442
 
Language eng
 
Relation http://131.114.27.37/index.php/AMS/article/view/350/pdf
 
Rights Copyright (c) 2019 Aerotecnica Missili & Spazio
 

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