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

Device (10) for the detachable connection of structural parts (80, 84), in particular 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) is rotated from a release position, wherein the clamping lever (16) is not engaged to the clamping pin (14), to a readiness position, wherein the clamping lever contacts the clamping pin in a non-locked position, by means of a first actuator actuating on the driving bushing;

• and wherein further movement of the clamping lever arrangement (12) will allow an eccentric section (28) of the eccentric shaft (20) to abut a surface of a stop section (76) of the driving bushing (18), making the clamping lever (16) to slidably move, allowing the clamping pin (14) to be received in a cavity (52) of the clamping lever (16) to lock the clamping lever arrangement, by means of a second actuator actuating on the eccentric shaft.