초록 ▼

The present invention relates to on-site repairs of a composite structure (10) such as an aircraft structure in which a concave recess (14) is machined in the damaged zone, a non-polymerized composite part (16) is set into said recess and part (16) is polymerized under pressure using tooling (18) co

The present invention relates to on-site repairs of a composite structure (10) such as an aircraft structure in which a concave recess (14) is machined in the damaged zone, a non-polymerized composite part (16) is set into said recess and part (16) is polymerized under pressure using tooling (18) comprising a stack of plates (32) that increase the pressure applied to the composite part. The present invention thus obtains invisible repairs with mechanical characteristics that are similar to those of the initial structure.

대표청구항 ▼

1. Method for on-site repair of a composite structure with a damaged zone, said method comprising the following stages:machining a concave recess in the damaged zone in a surface of the structure; setting a non-polymerized composite part in the recess, the shape of said composite part matching that

1. Method for on-site repair of a composite structure with a damaged zone, said method comprising the following stages:machining a concave recess in the damaged zone in a surface of the structure; setting a non-polymerized composite part in the recess, the shape of said composite part matching that of the recess; polymerizing the said composite part in situ using a vacuum created inside a bladder that is connected around the composite part to form a leaktight seal with said surface of the composite structure after means for increasing the pressure applied to the composite part have been interposed between the part and the bladder; heating the composite part; and interposing a stack of plates between the bladder and composite part, wherein the a plate proximate to the bladder has a surface area greater than a surface area of a plate proximate to the composite part.