基本信息:
- 专利标题： THERMOPLASTIC COMPOSITE WINDOW PANEL FOR AIRCRAFT APPLICATIONS
- 专利标题（中）：用于飞机应用的热塑复合窗面板
- 申请号：PCT/IB2010055128 申请日：2010-11-11
- 公开(公告)号：WO2011058514A2 公开(公告)日：2011-05-19
- 发明人： KELLER HANS-PETER , BAMERT-FALLEGGER RETO , SAJIC PETER JAMES
- 申请人： PELZER MARC , KELLER HANS-PETER , BAMERT-FALLEGGER RETO , SAJIC PETER JAMES
- 专利权人： PELZER MARC,KELLER HANS-PETER,BAMERT-FALLEGGER RETO,SAJIC PETER JAMES
- 当前专利权人： PELZER MARC,KELLER HANS-PETER,BAMERT-FALLEGGER RETO,SAJIC PETER JAMES
- 优先权： US61741609 2009-11-12
摘要：
An aircraft trim panel structure includes a thermoplastic resinated quadraxial fiberglass lay-up prepreg first open structure skin layer having at least a 28 % open area. A thermoplastic resinated quadraxial fiberglass lay-up prepreg second open structure skin layer has at least a 28 % open area. An open structure core layer having at least a 28 % open area is sandwiched between the first open structure skin layer and the second open structure skin layer. The first open structure skin layer, the second open structure skin layer and the open structure core layer are formed into a three dimensional shape corresponding to the aircraft trim panel.
摘要（中）：
飞机装饰板结构包括具有至少28％开放面积的热塑性树脂化四面体玻璃纤维铺层预浸料坯第一开放结构表皮层。 热塑性树脂化四面体玻璃纤维层叠预浸料第二开放结构表皮层至少具有28％的开放面积。 具有至少28％开放面积的开放结构的核心层夹在第一开放结构表皮层和第二开放结构表皮层之间。 第一开放结构表皮层，第二开放结构表皮层和开放结构芯层形成为对应于飞行器装饰板的三维形状。