Method repairing hole formed in composite material panel of aircraft to connect panel to beams through e.g. screw, involves pressing portion of panel surrounding hole, so that panel is compressed in direction of transverse axis of hole

摘要

The method involves placing a hole (16) that is formed in a composite material panel (10) in an injection volume (V) of resin in a water-tight manner. The resin is injected into the injection. A portion of the composite material panel surrounding the hole is pressed, so that the composite material panel is compressed in a direction of a transverse axis (A) of the hole, where the transverse axis is approximately perpendicular to a bedding plane of the composite material panel. The resin is heated after pressing the composite material panel. An independent claim is also included for a device for repairing a hole formed in a composite material panel.