Patent ID: 8220745
Filing Date: 2012-07-17
Classification: B64C,Y02T

Abstract:
1. Connection arrangement for connecting a first and second reinforcing element of an aircraft or spacecraft, wherein the reinforcing elements each have a profiled cross-section comprising at least one foot portion and at least one web portion and are spaced from one another at their end connection faces by a strap element, with: at least one foot portion connection element, which can be adjusted and firmly joined on one side to the geometric shape of the foot portion of the first reinforcing element, on the other side to the geometric shape of the foot portion of the second reinforcing element and to the interposed strap element; and at least one web coupling element, which can be adjusted and firmly joined on one side to the geometric shape of the web portion of the first reinforcing element, and on the other side to the strap element.