Patent ID: 7905029
Filing Date: 2011-03-15
Classification: B64C,B64D,B64F

Abstract:
1. An adjustment device for the alignment of supporting parts on structures having inherent dimensional tolerances in an aircraft fuselage, by means of joining surfaces, wherein a first joining surface comprises a plurality of positive shapes, each positive shape of the plurality of positive shapes being formed as a pointed body, and a second joining surface opposite the first joining surface comprises a plurality of negative shapes, each negative shape of the plurality of negative shapes being formed as a cavity, wherein the positive shapes engage corresponding negative shapes in a form fit, wherein the positive shapes and the negative shapes in each case are arranged in a cross grid for an adjustment movement parallel to a surface plane of the respective cross grid, and wherein the positive shapes and negative shapes in each case represent individual pixels within the respective cross grid, so that a smallest possible adjustment travel between the first joining surface and the second joining surface is determined by a base size of each positive shape and each negative shape.