发明名称 |
METHOD FOR CONNECTING A FIBER COMPOSITE COMPONENT TO A STRUCTURAL COMPONENT OF AN AIR AND SPACECRAFT, AND A CORRESPONDING ARRANGEMENT |
摘要 |
The invention relates to a method for connecting a fiber composite component (2) to a structural component (3) of an air and spacecraft, wherein a metal foil (4) is provided between the fiber composite component (2) and the structural component (3) as a transverse reinforcement element. Said foil is designed having at least one anchoring segment (7) protruding from the surface (9) facing the fiber composite component (2), and inserted between the fiber composite component (2) and the structural component (3). A corresponding arrangement is produced according to said method. |
申请公布号 |
WO2011069899(A2) |
申请公布日期 |
2011.06.16 |
申请号 |
WO2010EP68802 |
申请日期 |
2010.12.03 |
申请人 |
AIRBUS OPERATIONS GMBH;PACCHIONE, MARCO;FURFARI, DOMENICO |
发明人 |
PACCHIONE, MARCO;FURFARI, DOMENICO |
分类号 |
|
主分类号 |
|
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|