Plastic-composite profiled girder, in particular a wing spar...

B - Operations – Transporting – 29 – C

Patent

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B29C 65/54 (2006.01) B29D 99/00 (2010.01) B29C 65/00 (2006.01) B29C 65/48 (2006.01) B29C 70/52 (2006.01) B64C 3/18 (2006.01) E04C 3/28 (2006.01) B29C 67/14 (1990.01) B29D 31/00 (2006.01)

Patent

CA 2115350

ABSTRACT OF THE DISCLOSURE The invention concerns a plastic composite profiled girder, in particular an aircraft wing spar, comprising at least two chords with bonding flanges and at least one web inserted into the bonding flanges and connecting the chords to each other. The chords are made from resin-impregnated rovings and the web is made from resin-impregnated wovens or layups, and the chords and web are joined to each other by adhesive bonding. The chords are produced by pultrusion, the web being inserted into the bonding flange of both chords and fixed there using a thixotropic adhesive. This construction ensures that the full flange bonding width is maintained even if the height of the component is varied.

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