The invention concerns a suspension pylon comprising: - at least one arm (3) for hanging a propulsive assembly (4) from the fuselage (2) of an aircraft (1), - an oil exchange circuit (70) configured to be connected to an oil pump (5) in the fuselage (2) and to the propulsive assembly (4) whose arm (3) ensures suspension, said circuit (70) comprising a feed line (72) and a return line (74), each of which is extended from the inside of said arm (3), - an intermediate shaft (6) extending into said arm (3), said shaft being configured to be driven by the propulsive assembly (4) whose arm (3) ensures suspension, and to drive the oil pump (5) in the fuselage (2), the arm (3) presenting a structure adapted to cool the oil exchange circuit near the arm (3).
REFROIDISSEUR D'HUILE INTEGRE AU PYLONE
25.08.2017
Patent
Elektronische Ressource
Französisch
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