发明名称 |
SKIN PANEL FOR AN AIRCRAFT FUSELAGE |
摘要 |
The invention relates to a skin panel (11) of an aircraft (1), comprising a laminate of at least one first metal sheet (40) and preferably first fiber-reinforced polymer layers (41) connected thereto. The skin panel (11) is connected to stiffening elements (4) made of a laminate of second metal sheets (40) and second fiber-reinforced polymer layers (41) connected thereto, provided that the second fiber-reinforced polymer layer comprises fibers having a modulus of elasticity in tension of greater than 110 GPa. The invention also relates to an aircraft or spacecraft provided with such skin sheets. |
申请公布号 |
EP2061697(A1) |
申请公布日期 |
2009.05.27 |
申请号 |
EP20070808551 |
申请日期 |
2007.08.24 |
申请人 |
ALCOA INC. |
发明人 |
ROEBROEKS, GEERARDUS HUBERTUS JOANNES JOZEPH;GUNNINK, JAN WILLEM;KROON, ERIK JAN |
分类号 |
B64C1/12;B32B15/08 |
主分类号 |
B64C1/12 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|