Method for assembling two assemblies such aircraft fuselage assemblies

摘要

This invention comprises two assemblies, such as for example, an aircraft fuselage assembly with a plurality of fixing members It relates to a method of assembling. The method, to use a drilling tool comprising the step of drilling a hole in the overlapping area through the centering hole 36 formed in the drilling grid 34 is mounted securely in the overlap zone, the drilling tool is here to create the support mozzarella, and therefore the contact surface comprises a conical expansion ring 56 to close contact with the mandrel. According to the invention, after in the centering hole in the ring has been locked, by displacing the mandrel is supported on the stacking section in the direction of and overlapping section through the centering hole to apply pressure to the overlap zone, the expansion ring and make This relative movement is applied between Marla.