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 |