Device and method for the detachable connection of structural parts, in particular in an aircraft

Abstract

The invention relates to a device (10) for the detachable connection of structural parts (80, 84) in an aircraft, comprising a clamping lever arrangement (12) associated with a first structural part (80) and a clamping pin (14) associated with a second structural part (84), wherein the clamping lever arrangement (12) comprises an eccentric shaft (20) rotatably mounted about a rotation axis (A) on the first structural part (80), a clamping lever (16) mounted eccentrically and swivellably with respect to the eccentric shaft (20), and a driving bushing (18) rotatably mounted relative to the eccentric shaft (20) about the rotation axis (A) and coupled in a geared manner to the clamping lever (16), wherein the clamping lever arrangement (12) can furthermore be displaced between a release position, a readiness position and a locking position, wherein the clamping lever (16) in the release position releases the clamping pin (14) and wherein the clamping lever (16) in the locking position engages the locking pin (14) in an interlocking positive manner on account of a relative rotation of the eccentric shaft (20) and driving bushing (18) as well as the clamping lever (16).

Dependencies are inferred from the claim text.