Patent ID: 9452445
Filing Date: 2016-09-27
CPC Classification: B05D,B22F,B29C,B64C,Y02T

Claim Text:
1. A method for producing an aircraft structure component having an outer skin provided with an aerodynamic outer surface, the method comprising: providing the aircraft structure component having the outer skin with the aerodynamic outer surface, wherein the aerodynamic outer surface of the outer skin includes at least one recess disposed therein; detecting a location of the at least one recess disposed in the aerodynamic outer surface of the outer skin by a recess detecting device; filling the at least one recess at the detected location on the aerodynamic outer surface of the outer skin with particles of a filling material, wherein the filling material comprises metal, and wherein the particles of the filling material are applied into the at least one recess by an ink jet printing device; and sintering, via a laser, the filling material disposed in the at least one recess for joining the particles of the filling material.