The invention relates to an air directing arrangement (8) for controlling flow of air at a compartment outlet (2e) of a fuselage of a rotorcraft. The air directing arrangement (8) comprises a continuous surface (9) that covers the compartment outlet (2e) outside the fuselage and forms a flow channel (17) for directing an air flow at the compartment outlet (2e); a first flow-through opening (9a) that is formed at a first position (8a) of the flow channel (17), wherein the first flow-through opening (9a) forms an air inlet area; and a second flow-through opening that is formed at a second position (8b) of the flow channel (17), wherein the second flow-through opening is arranged downstream of the first flow-through opening (9a) in the predetermined flow direction, and wherein the second flow-through opening forms an air outlet area; wherein the air inlet area is smaller than the air outlet area.


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    Title :

    AN AIR DIRECTING ARRANGEMENT FOR CONTROLLING AIRFLOW AT AN OUTLET


    Additional title:

    LUFTLEITANORDNUNG ZUR STEUERUNG DES LUFTSTROMS AN EINEM AUSLASS
    AGENCEMENT D'ORIENTATION D'AIR POUR RÉGULER UN ÉCOULEMENT D'AIR AU NIVEAU D'UNE SORTIE


    Contributors:

    Publication date :

    2025-04-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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