Patent ID: 9421746
Filing Date: 2016-08-23
CPC Classification: B32B,B64C,B64F,C09J,F16B,Y02T,Y10T

Claim Text:
1. An apparatus for joining parts to be joined which are subject to tolerance in the aerospace sector, comprising: a plurality of uniform shape elements which are connected together in planar manner and which are arranged in a first region of a surface of a first part to be joined; and a first adhesive layer, which is applied onto the plurality of uniform shape elements and in a second region of the surface of the first part to be joined, such that the first adhesive layer is in contact with the surface of the second part to be joined, the first part to be joined being connected in planar manner to the second part to be joined, wherein the plurality of uniform shape elements are completely covered by said first adhesive layer such that a joint gap formed between the first and second parts to be joined is filled by means of the plurality of uniform shape elements arranged on the surface of the first part to be joined completely covered by the first adhesive layer.