A core compartment ventilation device is provided. The core compartment ventilation device comprises a fireproof sealing member (202) for substantially sealing a core compartment (66) in a nacelle (34) for a gas turbine engine (20) and a chimney (204) configured to be in fluid communication with the fireproof sealing member (202) for conducting hot air from the core compartment (66) to the external atmosphere via the fireproof sealing member (202). A gas turbine engine (20) and nacelle (34) including the core compartment ventilation device are also provided.
CORE COMPARTMENT VENTILATION DEVICES FOR NACELLES OF GAS TURBINE ENGINES FOR COOLING A CORE COMPARTMENT OF A GAS TURBINE ENGINE
KERNFACHBELÜFTUNGSVORRICHTUNGEN FÜR GONDELN VON GASTURBINENMOTOREN ZUM KÜHLEN EINES KERNFACHS EINES GASTURBINENMOTORS
DISPOSITIFS DE VENTILATION DU COMPARTIMENT CENTRAL DE NACELLES DE TURBINE À GAZ POUR REFROIDIR LE COMPARTIMENT CENTRAL D'UNE TURBINE À GAZ
2019-08-07
Patent
Electronic Resource
English
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