Composite Structure Utilization - Commercial Airplanes

2005-01-3315

10/03/2005

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
The advantage of higher strength to weight and higher stiffness to weight ratios for composite structure compared to metallic structure is well known in the aerospace industry, especially to commercial airline world. Its increased usage in the airplane structure is a direct reflection of the benefit in reduction of operating costs by lowering the fuel usage. This factor turned out to be more important for the airlines after the September 11, 2001 incident and also due to the increase in fuel prices. Besides reduction in the operating costs, airlines are seeking ways to reduce their maintenance costs. Most of the damage to the aluminum structure airplanes is attributed to corrosion. The non-metallic composite structure has an excellent property of resistance to corrosion. The structure is more damage tolerant due to the absence of fastener holes. As a result, its increased usage serves the airlines by lowering the maintenance and inspection costs.
Meta TagsDetails
DOI
https://doi.org/10.4271/2005-01-3315
Pages
16
Citation
Sheth, N., and Roach, D., "Composite Structure Utilization - Commercial Airplanes," SAE Technical Paper 2005-01-3315, 2005, https://doi.org/10.4271/2005-01-3315.
Additional Details
Publisher
Published
Oct 3, 2005
Product Code
2005-01-3315
Content Type
Technical Paper
Language
English