A damage recovery system of a fuselage (1) of an aircraft (3), comprising: a tank (8) containing a polyurethane foam; a main duct (10a) fluidically coupled to the tank to receive the foam; secondary ducts (10b) fluidically coupled to the main duct; and distribution means (12) adapted to allow an outflow of the foam from the secondary ducts. Graphene powder can be mixed and added to the polyurethane foam. In flight, a possible leak (crack or hole) in the fuselage is plugged by the polyurethane foam with graphene powder.
СИСТЕМА ДЛЯ УЛУЧШЕНИЯ ПРОЧНОСТИ КОНСТРУКЦИИ САМОЛЕТА И САМОЛЕТ, СОДЕРЖАЩИЙ ТАКУЮ СИСТЕМУ
2020-05-18
Patent
Elektronische Ressource
Russisch
СИСТЕМА НЕЗАВИСИМОЙ ПОДВЕСКИ И КРАН, ИМЕЮЩИЙ ТАКУЮ СИСТЕМУ
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