DEVICE AND METHOD FOR THE DETACHABLE CONNECTION OF STRUCTURAL PARTS, IN PARTICULAR IN AN AIRCRAFT

摘要

Device (10) comprises a tension lever arrangement (12) assigned to a first component and a clamping pin (14) assigned to a second component. The clamping lever arrangement has an eccentric shaft (20) rotating about a rotary axis on the first component, a clamping lever (16) pivoting on the shaft and a bushing (18) coupled with the clamping lever. The clamping lever arrangement can be displaced between a release position, a ready position and a locking position. The clamping lever releases the clamping lever into the release position. An independent claim is also included for a method for detachedly connecting components in an aircraft using the above device. Preferred Features: The bushing pivots on the shaft. The clamping lever pivots on an eccentric section of the shaft relative to the rotary axis.