| 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 fra me (1) comprises multiple substructures (16-19) welded to one another and has a core (17) comprising a unidirectional-running webbing.
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