| 摘要 |
<p>Joint attaching a structural element (10) to a composite part (20) comprising a metallic attachment (40), this joint being subjected to a fire source on one of its sides, the fire side, the joint comprising a retaining device (50) locate at the side of the joint opposite to the fire side, the cold side, the retaining device (50) comprising a first surface (51) that is in contact with the metallic attachment (40), and a second surface (52) which is in contact with the composite part (20), the second surface (52) having a bigger area than the area of the first surface (51), the retaining device (50) being made of a material with a high thermal conductivity. The invention also refers to an aircraft comprising such a joint.</p> |
