A component for a structure of an aircraft interior, wherein at least a portion of the component extends between a first point and a second point, defining a longitudinal axis of the component. The component includes at least one bushing. The at least one bushing is located at the first point and/or the second point. The component further includes a fibrous material that extends between the first point and the second point. The component further includes a thermoplastic that at least partially encases the at least one bushing and the fibrous material.
COMPONENT FOR AIRCRAFT INTERIORS
2024-10-10
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Engineering Index Backfile | 1941
|High performance composites for aircraft interiors; HPC aircraft interiors conference review
British Library Conference Proceedings | 2014