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1.
公开(公告)号:US20190135444A1
公开(公告)日:2019-05-09
申请号:US16180132
申请日:2018-11-05
申请人: LEONARDO S.P.A.
摘要: A damage recovery system of a fuselage of an aircraft, comprising: a tank containing a polyurethane foam; a main duct fluidically coupled to the tank to receive the foam; secondary ducts fluidically coupled to the main duct; and distribution means 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.
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公开(公告)号:US20180328895A1
公开(公告)日:2018-11-15
申请号:US15972982
申请日:2018-05-07
申请人: LEONARDO S.p.A.
IPC分类号: G01N29/24
CPC分类号: G01N29/2431 , B63B5/24 , B64C2001/0072 , B64D2045/0085 , B64F5/60 , G01N29/043 , G01N29/07 , G01N29/2475 , G01N2291/0231 , G01N2291/0258 , G01N2291/0289 , G01N2291/0421 , G01N2291/101 , G01N2291/2638 , G01N2291/2694
摘要: Non-destructive inspection device, comprising: a first structural layer; a second structural layer coupled to the first structural layer; a chamber sealed between the first and second structural layers, containing a gas; and an active region, housed in the chamber, of a Graphene-based material. In a first operating condition, an AC electric current is fed to the active region and generates by thermoacoustic effect a first acoustic wave propagating away from the chamber. In a second operating condition, a second acoustic wave, generated by a reflection of the first acoustic wave, is received at the chamber and causes a variation in pressure and, consequently, a variation in the temperature of the gas contained in the chamber generating, by means of the thermoelectric effect, an electrical signal in the active region.
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