发明名称 Method for producing an aircraft structure component having an outer skin provided with a smooth outer surface
摘要 A method for producing an aircraft structure component is disclosed the component having an outer skin provided with a smooth outer surface. The method includes providing an aircraft structure component having an outer skin including at least one recess, detecting the location of said at least one recess by a recess detecting device, and filling said at least one recess at the detected location with particles of a filling material, said particles of filling material being applied into said at least one recess by an ink jet printing device.
申请公布号 US9452445(B2) 申请公布日期 2016.09.27
申请号 US201314016826 申请日期 2013.09.03
申请人 Airbus Operations GmbH 发明人 Frankenberger Eckart
分类号 B05D3/06;B64C21/10;B22F3/105;B29C67/00;B64C1/00;B64C3/26 主分类号 B05D3/06
代理机构 Jenkins, Wilson, Taylor & Hunt, P.A. 代理人 Jenkins, Wilson, Taylor & Hunt, P.A.
主权项 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.
地址 Hamburg DE