| 摘要 |
Disclosed is a fastening system for quick-releasably fastening interior components in the cabin of an aircraft. Said fastening system comprises a perforated profiled element (1) and a quick-change fitting (2) that can be releasably connected thereto. The perforated profiled element has at least one mounting hole (3) while the quick-change fitting encompasses a housing (4), at least one locking rocker (12) with a first locking projection (16) that is disposed at the end thereof, a second locking projection (16), and a tappet which is guided within the housing to be movable between two final positions. The tappet has an expansion wedge and at least one sliding surface with an opening cam. In the first final position of the tappet, the expansion wedge extends between the two locking projections (16) and forces the same apart, while in the second final position of the tappet, an opposite cam which is arranged on the locking rocker, on the final tappet section located across from the locking projection, rests against the opening cam, the expansion wedge is retracted from the area located between the two locking projections, and the two locking protrusions substantially rest against each other. |
