The invention relates to a fluid duct system for thermal management and/or ventilation in a compartment containing at least one temperature sensitive target within a turbo engine, said turbo engine comprising a first spatial area within the turbo engine through which a fluid flows during operation of the turbo engine, characterized by a fluid duct device (3) connecting the first spatial area (1) with a second spatial area (2) having a lower pressure than the first spatial area (1) during operation of the turbo engine (7), so that a pressure gradient is present in the fluid duct device (3) and a flow of fluid from the first spatial area (1) towards the second spatial area (2) is generated resulting in a pressure gradient in the compartment (11) and therefore in a flow of fluid for thermal management and/or ventilation of the compartment (11).
TURBO ENGINE WITH A FLUID DUCT SYSTEM
TURBOMASCHINE MIT EINEM FLUIDLEITUNGSSYSTEM
TURBOMACHINE ÉQUIPÉE D'UN SYSTÈME DE CONDUIT DE FLUIDE
2019-08-07
Patent
Electronic Resource
English