An aircraft panel assembly with a panel and a plurality of stiffeners on the panel is disclosed. Each stiffener has an attachment part attached to the panel and a structural part spaced apart from the panel. A rib foot beam crosses the stiffeners at a series of intersections. At each intersection the rib foot beam is located between the panel and the structural part of a respective one of the stiffeners.
AIRCRAFT PANEL ASSEMBLY
27.01.2022
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2025
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