| 摘要 |
The window frame (1) includes at least one vertical flange (4) perpendicularly arranged between at least one outer flange (2) and at least one inner flange (3) such that the flanges are made of a fiber-reinforced resin. The vertical flange connects to an aircraft structure via one of the outer and inner flanges. An independent claim is also included for a window frame manufacturing method. |
