This application claims priority to European patent application 07117229.0 filed 26 Sep. 2007.
1. Field of the Invention
The present invention relates generally to a method for forming an elongate, hollow article of a fiber-reinforced composite material.
The invention also relates to a tool for forming an elongate, hollow article of a fiber-reinforced composite material, comprising an elongate, metallic tool bar having a first end and a second end.
2. Description of Related Art
When forming elongate, hollow articles of fiber-reinforced composite material, such as hollow beams or the like for the aircraft manufacturing industries, a metallic core or bar is often used as a mandrel or tool, around which a plurality of layers of a resin-impregnated tape (so called “prepreg”) is applied by winding it in an overlapping manner to form a laminated, semi-finished article. After curing of this composite article in a subsequent heat-treatment step, e.g. in an oven or autoclave, the cured article is cooled together with the tool bar. In the cooling phase, normally in room temperature, the tool bar shrinks to a certain degree, i.e. the cross-sectional area and the length of the tool bar is somewhat reduced, whereas the dimensions of the cured article remain substantially unchanged. In some cases, especially where the article and the tool bar is slightly curved in one or two directions and has a lengthwise tapered configuration, the shrinkage of the tool bar may cause undesired engagement between the tool bar and the cured article at certain locations along the tool bar due to uncontrolled mutual longitudinal movements of the tool bar and the article during the cooling phase. This may irrevocably damage the article at certain locations when dismantling the same from the tool bar.
It is a primary object of the present invention to provide an improved method for forming an elongate, hollow article of a fiber-reinforced composite material which eliminates the above-mentioned drawback of the prior art methods. Owing to the arrangement of the uncured article laminate on the tool bar such that during the heat-treatment and the cooling phases one end of the laminate engages a support surface or is supported by a support surface of an anvil fixed to the tool bar, the direction of movement of the cured article relative to the tool bar can be controlled to be in only one suitable longitudinal direction which does not affect the cured article.
According to another aspect of the invention there is provided a specific tool for carrying out the method of the invention, i.e. for forming an elongate, hollow article of a fiber-reinforced composite material, which ensures a controlled longitudinal movement of the cured article relative to the tool bar during the shrinkage phase thereof and a subsequent damage-free dismantling of the cured article from the tool bar.
Further details of the method and the tool of the invention will be described in the following detailed description with reference to the accompanying drawing.
In manufacturing for example an elongate hollow beam for an inner support structure of an aircraft control surface a plurality of layers 20 of resin-impregnated fiber-reinforced web material (“prepreg”) are applied on the tool bar 14, e.g. by a tape-laying machine (not shown) winding overlapping layers 20 around the tool bar 14. The inner end of the laminated, uncured article 12 is placed in engagement with the radial support surface 18, is supported by the radial support surface 18 or is lying against the radial support surface 18 of the anvil 16. Then, the tool 10 and the uncured article 12 is heated in an oven or an autoclave (not shown) in order to cure the article 12 on the tool bar 14.
After the curing step the tool 10 and the cured article 12 are allowed to cool in room temperature. As shown exaggerated in
Further, the present invention relates to the use of the tool 10 described above, which has an elongate, metallic tool bar 14 with a first end and a second end, wherein the tool bar 14 is provided with an anvil 16 at the first end thereof, said anvil 16 having a fixed surface 18 protruding radially from the tool bar 14 for forming an article of a fiber-reinforced composite material by the steps of:
Number | Date | Country | Kind |
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07117229 | Sep 2007 | EP | regional |
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1260349 | Nov 2002 | EP |
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Number | Date | Country | |
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20090107619 A1 | Apr 2009 | US |