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 (126) coupled to the aircraft structure, a piston (128)located at least partially within the outer cylinder (126) and coupled to the interior aircraft monument, and a compressed gas located in a volume defined by the piston (128)and the outer cylinder (126).
LOAD ABSORBING TIE ROD FOR AIRCRAFT STRUCTURE INTEGRATION
LASTAUFNEHMENDE ZUGSTANGE ZUR INTEGRATION EINER FLUGZEUGSTRUKTUR
TIRANT D'ANCRAGE ABSORBANT LA CHARGE POUR INTÉGRATION DE STRUCTURE D'AÉRONEF
2023-10-04
Patent
Electronic Resource
English
LOAD ABSORBING TIE ROD FOR AIRCRAFT STRUCTURE INTEGRATION
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