A lightweight overhead stowage compartment comprising a self-supporting hull having an open cross-section forming a stowage space and an opening to the stowage space, wherein in a longitudinal direction of the self-supporting hull any section of the self-supporting hull has an open end in the front and rear. The stowage compartment includes a vertical connector configured to be placed into the stowage space, wherein the vertical connector is mounted to the self-supporting hull at vertical sides of the vertical connector in a force transferring manner. At least one lid is mounted at an arbitrary section of the self-supporting hull and configured to close the opening to the stowage space.
LIGHTWEIGHT OVERHEAD STOWAGE COMPARTMENT AND METHOD OF INSTALLING THE SAME
2024-10-03
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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