| 摘要 |
The invention relates to a device (1) for joining torsion boxes (5, 6) of aircraft structures, said structures carrying fuel therein, characterized in that the mentioned device (1) comprises three sides (2, 3, 4) by means of which it is secured to the inner part of the structural parts of the joint of the torsion boxes (5, 6) of the aircraft in a permanent manner, said device (1) thus closing the joint of the boxes (5, 6) and preventing possible fuel leaks, the device (1) being a non-structural component of the mentioned joint since it does not withstand the loads of the structure of the joint of torsion boxes (5, 6). |
