| 摘要 |
<p>The invention relates to a Galley container (1) for use in an aircraft, comprising at least two container sidewalls (6), a container floor element (7) and a container ceiling element (8), forming a hollow inner shell casing (2) with a circumferential first rim (12) and a circumferential second rim (12'). The composite tape (11) is spun around the inner shell casing and along the circumference of the rims, forming at least part of a construction layer (5) of the galley container. The composite tape comprises at least one fibre and a matrix material.</p> |
