The invention concerns a tank retainer for retaining a tank in the fuselage of an aircraft which includes, between the tank and a frame rigidly connected to the fuselage of the aircraft, a hinged retaining means and a fastening rod on which said hinged retaining means is mounted. Advantageously, the hinged retaining means is intended to be connected to a rear end of the tank and the fastening rod is suitable for being mounted on the frame rigidly connected to the fuselage of the aircraft and, preferably, the hinged retaining means comprises a ball joint.
DISPOSITIF DE RETENUE D'UN RESERVOIR DANS UN AERONEF
2016-07-15
Patent
Elektronische Ressource
Französisch
ENSEMBLE CONSTITUE D'UN RESERVOIR ET D'UN DISPOSITIF DE RETENUE DU RESERVOIR DANS UN AERONEF
Europäisches Patentamt | 2020
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