An aircraft assembly may comprise an interior aircraft monument, an aircraft structure, and a load absorbing tie rod coupled to the interior aircraft monument and the aircraft structure. The load absorbing tie rod may include an outer cylinder coupled to the aircraft structure, a piston located at least partially within the outer cylinder and coupled to the interior aircraft monument, and a compressed gas located in a volume defined by the piston and the outer cylinder.
LOAD ABSORBING TIE ROD FOR AIRCRAFT STRUCTURE INTEGRATION
28.09.2023
Patent
Elektronische Ressource
Englisch
LOAD ABSORBING TIE ROD FOR AIRCRAFT STRUCTURE INTEGRATION
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