Repair of composite laminates
AssigneeBritish Aerospace Public Limited Company
InventorGeoffrey McBroom
Life of this patent
Estimating the term…
Abstract
A patch of fibre reinforced plastics composite material, a repair kit including such a patch and a method of using such a patch and repair kit are provided. The patch (1) is for attachment to a surface (17) of a fibre reinforced plastics composite structure (11) over an area of damage (10) to the structure. The patch defines an outer surface (3), a bonding surface (4) opposed thereto and a peripheral edge. The patch includes fibre reinforcement and plastics matrix material with the latter being in a final state of hardness. The patch defines a series of small apertures (6) therethrough to allow the passage of gases and other matter through the patch to prevent entrapped air weakening the repair.
Claims22
A patch of fiber reinforced plastics composite material for attachment to a surface of a fiber reinforced plastics composite structure over an area of damage to the structure, said patch defining an outer surface, a bonding surface opposed thereto and a peripheral edge, said patch including fiber reinforcement and plastics matrix material and said plastics matrix material being in a substantially final state of hardness, wherein said patch defines a series of apertures therethrough to allow the passage of matter therethrough during bonding of said patch to the structure, and said patch includes a perforated film adhered to said outer surface.
A method of repairing an area of damage to a surface of a fiber reinforced plastics composite structure with a patch, said structure including at least a monolithic laminate and said area of damage including a crater at least in said laminate, said patch is made of fiber reinforced plastics composite material for attachment to said surface of said fiber reinforced plastics composite structure over said area of damage to the structure, said patch defining an outer surface, a bonding surface opposed thereto and a peripheral edge, said patch including fiber reinforcement and plastics matrix material, said plastics matrix material being in a substantially final state of hardness, said patch defines a series of apertures therethrough to allow the passage of matter therethrough during bonding of said patch to the structure, the method including the steps of:
- applying to surfaces to be bonded and introducing into said crater liquid adhesive;
- leveling off said adhesive to stand slightly proud of said surface of said structure whilst substantially filling said crater;
- applying said patch to said surface so as to cover said crater;
- and
- extracting any excess adhesive and gas from beneath said patch through said apertures in said patch and hardening said adhesive to bond said patch in position and complete the repair.
Dependencies are inferred from the claim text.