Ventilation of an internal compartment of a fairing device of a propulsion assembly in an aircraft moving at low speed on the ground or when it is stopped cannot be provided optimally using a conventional dynamic air intake. To solve this problem, the use of a fan housed within the internal compartment is proposed, for which the fan propeller can alternately be coupled to an accessory gear box to drive the fan propeller, and uncoupled from the accessory gear box when it is unnecessary to drive the fan propeller or when it represents a danger.


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    Title :

    Dispositif de carénage pour ensemble propulsif d'aéronef comprenant un compartiment intérieur équipé d'un ventilateur


    Additional title:

    Fairing device for aircraft propulsion assembly including an inner compartment provided with a fan
    Verkleidungsvorrichtung für das gesamte Antriebssystem eines Luftfahrzeugs, die ein Innenfach mit einem Ventilator enthält


    Contributors:

    Publication date :

    2016-05-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT