发明申请
- 专利标题： METHOD AND A DEVICE FOR THE MANUFACTURE OF A STIFFENING STRUCTURE FOR AN AIRCRAFT FUSELAGE SEGMENT, AND ALSO A STIFFENING STRUCTURE
- 专利标题（中）： 用于制造用于飞机熔接部分的强化结构的方法和装置，还有结构强化
-
申请号： US12980479申请日： 2010-12-29
-
公开(公告)号： US20110186683A1公开(公告)日： 2011-08-04
- 发明人: Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau , Hartmut Herter , Kevin Danke
- 申请人： Georg Lonsdorfer , Hauke Seegel , Klaus Rode , Andreas Pau , Hartmut Herter , Kevin Danke
- 申请人地址： DE Hamburg
- 专利权人： AIRBUS OPERATIONS GMBH
- 当前专利权人： AIRBUS OPERATIONS GMBH
- 当前专利权人地址： DE Hamburg
- 优先权： DE102009060706.4 20091229
- 主分类号： B64C1/00
- IPC分类号： B64C1/00 ; B29C70/30 ; B29C70/54
摘要：
A method for stiffening a skin field of an aircraft fuselage includes providing a skin field for an aircraft fuselage, manufacturing an integral lattice-shaped stiffening structure including a plurality of longitudinal stiffeners and connecting the stiffening structure to the skin field. The manufacturing can include the use of a tool mold having a plurality of longitudinal recesses configured to form longitudinal stiffeners and a plurality of sunken areas disposed between the longitudinal recess. The sunken areas are configured for forming respective mounts that are configured for connection to circumferential stiffeners.
公开/授权文献
信息查询
