An aeroengine 100 comprising a cowling 101 with at least two zones 1, 2 enclosed by the cowling 101, wherein a first zone 1 and at least one second zone 2 are separated by a wall 3, the cowling 101 circumferentially enclosing a core engine 104, surrounded by a bypass duct comprising a radially outer fairing 118 and a radially inner fairing 111, the at least one second zone 2 to receive fluid leakages from at least one supply line for fluids 5, 6, 7, entering the at least one second zone 2 through at least one fluid passage in a section of the radially outer fairing of bypass duct 118, the at least one second zone 2 comprises at least one duct 4 connecting the at least one second zone 2 to the environment (E).
Aeroengine and process of operating an aeroengine
2025-05-07
Patent
Electronic Resource
English
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