Manufacture of composite laminate aircraft landing gear...

B - Operations – Transporting – 29 – C

Patent

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B29C 44/16 (2006.01) B29C 44/12 (2006.01) B29C 70/08 (2006.01) B64C 25/00 (2006.01) B64C 25/16 (2006.01) B64C 25/32 (2006.01)

Patent

CA 2223543

A method of forming an aircraft landing gear strut fairing/debris protector and such a fairing/debris protector are provided. The fairing/debris protector comprises first and second fibre reinforced plastics skin elements (21, 23) with a foamed core (27) between them. The method includes the steps of providing a tool having a tool surface (15, 20) to form each said skin element, forming a lay-up (21, 23) on each said tool surface of fibrous reinforcing material and plastics matrix material and allowing the matrix material at least partly to harden, positioning the tools (8, 13) such that the two skins (21, 23) are supported in their final relationship to each other and introducing a foaming resin (27) between the skins to form a foam core.

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