A new manufacturing methodology, termed shape-inclusive lay-up, has been de
veloped for manufacture of dry-fibre preforms using non-crimp fabric (NCF).
Shape-inclusive lay-up enables preforms for three-dimensional components t
o be produced and stored flat, introducing the shape only when the preform
is loaded into the mould. The lay-up process is jigless, and complex compon
ents can be produced as a single preform, reducing both preform production
and moulding times. Aerospace components with varying degrees of complexity
can be manufactured using this technique, including skin components and re
inforcement structures. A range of technologies has been developed for auto
mating the lay-up process. This paper focuses on the requirements of the jo
ining process. The various methods of ply attachment investigated are descr
ibed. The method that both satisfies the process requirements and is suitab
le for automation is single-sided stitching using a loose chain stitch. The
stitching process has been studied and implemented for the production of d
ry carbon preforms. A stitching device in the form of a robotic end-effecto
r is described. Prototype testing is detailed and the results of these test
s are discussed.