| 摘要 |
A window frame (1) for installation in the exterior shell (5) of an aircraft, which comprises in each case at least one outer flange (2), one inner flange (3), and one vertical flange (4) arranged perpendicular and between these flanges, is manufactured from a fiber-reinforced thermoplastic material, by, first, manufacturing a semifinished part from webbing and thermoplastic material, which subsequently is deep-drawn in a molding tool. The window frame (1) comprises multiple substructures (16-19) welded to one another and has a core (17) comprising a unidirectional-running webbing.
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