Manufacture of Composite Panels with J-Shape Stiffeners |
| |
Authors: | F Elaldi S Lee R F Scott |
| |
Affiliation: |
a Technical Department, Turkish Land Forces, Ankara, Turkey
b Structures and Materials Laboratory, Institute for Aerospace Research National Research Council of Canada, Ottawa, Ontario, Canada |
| |
Abstract: | The use of composite materials in primary structure of aircraft is becoming more common. Stiffened composite panels have been designed for a variety of load carrying conditions in aircraft. In this, study, manufacturing techniques for stiffened composite panels were reviewed and discussed. Co-curing and secondary bonding manufacturing techniques were used to produce four stiffened composite panels. Experience gained with these techniques is discussed. Ultrasonic C-scan inspection was carried out to detect any defects in the panels. These panels were tested in compression to verify their structural capability in the post-buckled state. This paper presents the details of the tool design concepts and manufacturing techniques, and identifies and discusses the advantages and disadvantages of each manufacturing technique. |
| |
Keywords: | |
本文献已被 InformaWorld 等数据库收录! |
|