Automatic fiber placement machines are known in the field of composite materials as making the manufacturing more efficient. They involve moving a fiber placement head past a tool, such as a mould, and depositing fiber tows on the tool, see e.g.

US6692681B1, US2007044896A1, WO2005105641A2, US7376480, EP1804146, EP1292522B1 or US20080156436A1. Automatic fiber placement machines are traditionally used for manufacturing relatively small parts. For making larger composite bodies, such as shells for wind turbine blades, special challenges occur from the large size of the tools used, the large amount of material that has to be fed, and the time that is needed for completion of the placement process.

The object of the invention is to make automatic manufacturing of composite parts better adapted to manufacturing of large composite parts. This object is reached with a composite body manufacturing apparatus comprising a mould and a fiber placement machine comprising at least two fiber placement heads, the fiber placement machine being adapted to move the fiber placement heads past the mould and to deposit with the heads on the mould respective plies, wherein the fiber placement heads are arranged so that they simultaneously and sequentially follow the same path of movement, so that a multilayered stack of plies can be provided by the simultaneous movement of the heads.

This means that a relatively thick layer of material can be provided by each movement of the machine. At the same time, the material for the plies can be kept relatively thin so that material handling before deposition in the mould is not complicated by thick materials.

Here a composite body means an item comprising a fiber reinforced plastic material, such as epoxy, polyester, vinylester or similar, reinforced with a fiber material, such as glass fiber, carbon fiber, aramid fiber or similar.

The object is also reached with a method according to claim 2. Below an embodiment of the invention will be described with reference to the drawings, in which fig. 1 shows a perspective view of a composite body

manufacturing apparatus according to one embodiment of the invention, fig. 2 shows a side view of a detail of the apparatus in fig. 1 , and fig. 3 shows a top view of plies provided in a mould.

Fig. 1 shows schematically a composite body manufacturing apparatus according to one embodiment of the present invention. The apparatus comprises a wind turbine blade spar cap mould 1 and an automated fiber placement machine 2. The machine 2 comprises three fiber placement heads 21, which, by means of a guide arrangement, can be moved in any direction along the surface of the mould 1. The guide arrangement comprises a gantry 2011 which bridges the mould 1, and is movable in a longitudinal direction along the mould 1 by means of rails 2012. The fiber placement heads 21 are arranged on the gantry so as to allow movements in other directions, e.g. transversely to the mould, vertically and rotationally.

In this embodiment the fiber placement heads 21 are all arranged on the same holder 27 of the machine 2, and each head 21 comprises a roller 21. A plurality of reels (not shown) is provided in the holder 27 of the machine 2, each with a respective fiber tow of pre-impregnated fibers. (Alternatively, dry fiber tows could be provided.) As can also be seen in fig. 2, the machine 2 is arranged so that while being moved, each fiber placement head 21 is fed a plurality of tows from respective reels, and it places the tows side by side so as to form a ply 26, on the mould. Each fiber placement head 21 is adapted to be forced, while moving, to the mould 1 , whereby the ply 26 is formed by each head 21. In the example shown in fig. 1 and fig. 2, the heads 21 are moved in a direction indicated by the arrow A2. The fiber placement heads 21 are arranged so that they follow, simultaneously and sequentially (one after the other), the same path of movement. Thereby, a multilayered stack 261 of plies 26 is provided by the simultaneous movement of the heads 21.

Referring to fig. 3, preferably simultaneously and sequentially deposited plies 26 overlap fully. In any case, simultaneously and sequentially deposited plies 26 overlap with an overlap width OL which is at least 50%, preferably at least 70%, more preferably at least 90%, of the width W of one of the plies. Fig. 3 shows only 2 plies, while fig. 1 and fig. 2 show simultaneous deposition of three plies. It should be noted that in other embodiments more than three piles can be deposited simultaneously.

As is known in the art, a heater (not shown) can be provided at the fiber placement heads 21 to heat the matrix of the fiber tows 24, 25 so as to make the fiber tows stick when deposited.