A fluid ice protection system for an aircraft includes a plenum back wall and a fluid delivery network. The plenum back wall is affixed to an interior surface of an inlet cowl of a nacelle of the aircraft to define a plenum between the interior surface and a front surface of the plenum back wall. The nacelle surrounds a rotor assembly of an aircraft propulsion system. The inlet cowl defines a plurality of perforations through a thickness of the inlet cowl. The perforations are fluidly connected to the plenum. The fluid delivery network is coupled to the plenum back wall and configured to supply an anti-ice liquid into the plenum for the anti-ice liquid to penetrate through the perforations onto an exterior surface of the inlet cowl along a leading edge section of the inlet cowl.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT FLUID ICE PROTECTION SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    2024-01-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    AIRCRAFT FLUID ICE PROTECTION SYSTEM

    RUST CHARLES WILLIAM | Europäisches Patentamt | 2024

    Freier Zugriff

    Protection of Aircraft Fluid Systems

    J. M. Metcalf / R. E. Roberts / S. D. Bridgeman | NTIS | 1968


    Aircraft interior protection system

    STENBERG NATHANIEL JAMES | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft stall protection system

    LEOPOLD DAVID DANIEL / WILSON DOUGLAS LEE / MILLS NIKOS DAMIAN | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft staircase protection system

    PARKS ROLF H | Europäisches Patentamt | 2018

    Freier Zugriff