Mechanical joints of carbon fibre composite materials has been the subject of exten sive research in the past decade. Theoretical as well as experimental studies are avail able. In this article the structural use of aramid is examined by an experimental analysis of mechanical joints in various types of laminates. The relationship between bearing strength and laminate type and thickness is investigated and the influence of the pitch/ diameter ratio is studied. The safe failure behaviour typical of aramid composites is demonstrated by testing riveted joints.
Get full access to this article
View all access options for this article.
References
1.
W.H.M. van Dreumel, High strength aramid as a structural materialDelft University of Technology. Technical Symposium "The design and use of kevlar in aircraft. October 1982, Geneva, Switzerland
2.
C.A.M. de Koning, The peel strength of aramid reinforced materialsDelft University of Technology. Memorandum M-429. June 1982, Delft.
3.
J.C. Dardelet, and W.H.M. van Dreumel , Design, fabrication and testing of an advanced composite access door for use in a lower wing panelDelft University of Technology. Report LR-335. October 1981, Delft.
4.
Th.de Jong, The influence of friction on the theoretical strength of pin-loaded holes in orthotropic platesDelft University of Technology . Report LR-350. March 1982, Delft.
5.
Jointing in Fibre Reinforced Plastics Symposium September 1978 , Imperial CollegeLondon.
