Abstract: A reconfigurable manufacturing cell (10) for use in a manufacturing system (100; 200), e.g. pilot line, comprises a plinth (12) and a table (14) disposed on top of the plinth (12). The plinth (12) is modular in construction having a plurality of plates (26a-26k) and/or blocks. In particular but not exclusively, the cell (10) further comprises a collaborative robot (16) and an industrial robot (18), the industrial robot (18) configured to receive a variety of different end effectors such as an end effector (22) configured to perform an automated fibre placement (AFP) operation.

Abstract: The invention relates to a method of manufacturing a three dimensional structure having an internal space, the method comprising the following steps: (a) arranging a preform of fibre reinforced material in a first configuration in which the preform is supported by a support structure; (b) selectively curing the preform when laid out on the support structure to produce an intermediate preform, the intermediate preform comprising at least two selectively cured portions interconnected by at least one non-selectively cured portion; and (c) moving the two selectively cured portions with respect to one another to form the three dimensional composite structure in which the two portions at least partially surround the internal space of the structure. A preform of fibre reinforced material for use in a method of manufacturing a three dimensional structure having an internal space also forms part of the invention.

Abstract: The invention relates to a structural member comprising: a core portion that defines at least one anchor point, the core having at least one surface, a fibre tow arranged in a closed loop on the surface of the core portion, the loop defining a boundary of a space which contains the at least one anchor point, and a protective shell formed from a woven fibre sheet material which covers the fibre tow, and in which the core, fibre tow and the protective shell are impregnated and bound together by a cured resin. The invention also relates to a method of constructing a structural member.

Abstract: The invention relates to a structural member comprising: a core portion that defines at least one anchor point, the core having at least one surface, a fibre tow arranged in a closed loop on the surface of the core portion, the loop defining a boundary of a space which contains the at least one anchor point, and a protective shell formed from a woven fibre sheet material which covers the fibre tow, and in which the core, fibre tow and the protective shell are impregnated and bound together by a cured resin. The invention also relates to a method of constructing a structural member.

Abstract: The invention relates to a method of manufacturing a three dimensional structure having an internal space, the method comprising the following steps: (a) arranging a preform of fibre reinforced material in a first configuration in which the preform is supported by a support structure; (b) selectively curing the preform when laid out on the support structure to produce an intermediate preform, the intermediate preform comprising at least two selectively cured portions interconnected by at least one non-selectively cured portion; and (c) moving the two selectively cured portions with respect to one another to form the three dimensional composite structure in which the two portions at least partially surround the internal space of the structure. A preform of fibre reinforced material for use in a method of manufacturing a three dimensional structure having an internal space also forms part of the invention.