| 摘要 |
Described is a system (10) for releasably connecting a fitting piece (20), such as an interior lining of an aircraft cabin, to a supporting structure (30), such as a fuselage. A structural holder (50) is fastened to the supporting structure (30). A two-piece plug-in holding mechanism (60) including a connecting pin (80) and a bushing piece (85) is fastened to the structural holder (50) and to an adapter module (40) which is fastened to the fitting piece (20). An electrical contact device (70) can be arranged between the bushing piece (85) of the plug-in holding mechanism (60) and the structural holder (50). The adapter module (40) is used for compensating the angle and the vertical position between the fitting piece (20) and the supporting structure (30). The adapter module (40) is a block of a solid material, the connecting surfaces of which extend at an angle from each other. The adapter module (40) is mounted such that the connecting surfaces are oriented at different angles and arranged at different distances from each other. In addition, during assembly, the adapter module (40) can be fastened so as to be partially lowered into the fitting piece (20) at different depths and, if required, also at a desired inclination. |
