摘要 |
The invention relates to a structural part (10, 20, 40) made of a composite material, comprising a ply (11, 21) of carbon fibres (12, 22) unidirectional along a first axis (13, 23), said part furthermore comprising a metal element (14, 29, 34, 41) aligned with said carbon ply along said first axis, said part being characterized in that it comprises a first area (15, 32, 33) of contact between the carbon ply and the metal element, said area lying substantially parallel to the first axis, so as to enable the transfer of heat and/or electricity between said carbon fibres and said metal element. Such a part may be used in a structure requiring good heat and/or electrical transfer properties in association with high strength and low weight. |
申请人 |
EUROPEAN AERONAUTIQUE DEFENCE AND SPACE COMPANY EADS FRANCE;ASPAS PUERTOLAS, JESUS;BERMUDEZ, MICHEL;FOUQUEMBERGH, MICHEL;MAISONNAVE, NICOLAS |
发明人 |
ASPAS PUERTOLAS, JESUS;BERMUDEZ, MICHEL;FOUQUEMBERGH, MICHEL;MAISONNAVE, NICOLAS |