An aircraft cargo restraint system includes an attenuator member fixed at two first attachment locations within a cargo storage compartment of a fuselage of an aircraft. The cargo restraint system also includes a cargo restraint configured to be coupled to the attenuator member at a second attachment location of the attenuator member, located between the two first attachment locations. The cargo restraint is configured to restrain cargo loaded on a cargo deck of the cargo storage compartment. The attenuator member is configured to deflect in response to a load applied to the attenuator member by the cargo restraint.
SYSTEM AND METHOD FOR RESTRAINING CARGO
SYSTEM UND VERFAHREN ZUM SICHERN VON LADUNG
SYSTEME ET PROCEDE DE RETENUE D'UNE CARGAISON
2021-06-23
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |