Manufacture of Composite Panels with J-Shape Stiffeners

Autor:	F. Elaldi, R. F. Scott, S. Lee
Rok vydání:	1995
Předmět:	Engineering Mechanics of Materials business.industry Mechanical Engineering Composite number General Materials Science Structural engineering business Load carrying Tool design Industrial and Manufacturing Engineering Secondary bonding
Zdroj:	Materials and Manufacturing Processes. 10:27-36
ISSN:	1532-2475 1042-6914
DOI:	10.1080/10426919508934996
Popis:	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.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b6ea2e4516f07a47e5260158f4da5e2b https://doi.org/10.1080/10426919508934996 Zobrazit plný text záznamu