A sealing device for an oil chamber of a turbojet

The invention relates to a sealing device for a housing (4, 5) formed by at least one rotating member (3, 15) and at least one static member (12, 13) of a turbojet engine (1) and for contain a suspension of lubrication oil droplets (h). The sealing device comprises at least one brush seal (14) with strands (17) juxtaposed, arranged to provide a seal between at least one rotating member (15) and at least one fixed member (12). This device is characterized in that it comprises means (12, 19, 20, 22, 23, 24, 25, 26, 30) of lubricating oil supply (h) of the brush seal (14) arranged for generating an oil flow (h) along its strands (17). The gasket (14) and resistant to coking.