An anti-icing protection system for an aircraft engine nacelle, the nacelle comprising an inner shroud, an air intake lip forming a leading edge of the nacelle, the protection system comprising a heat exchanger device including at least one heat pipe configured to transfer heat emitted by a heat source to the inner shroud.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft engine nacelle comprising a system of ice protection


    Contributors:

    Publication date :

    2023-05-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    AIRCRAFT ENGINE NACELLE COMPRISING ICE PROTECTION SYSTEM

    PORTE ALAIN / PONS FRANCOIS / ALBET GREGORY et al. | European Patent Office | 2020

    Free access

    AIRCRAFT ENGINE NACELLE COMPRISING A SYSTEM OF ICE PROTECTION

    PORTE ALAIN / PONS FRANÇOIS / ALBET GREGORY et al. | European Patent Office | 2020

    Free access

    AIRCRAFT ENGINE NACELLE COMPRISING AN ANTI-ICING PROTECTION SYSTEM

    PORTE ALAIN / LALANE JACQUES / ALBET GREGORY et al. | European Patent Office | 2020

    Free access


    Aircraft nacelle comprising sealing system and aircraft comprising such nacelle

    SAMMITO LAURENT / GELIOT JEAN / THERON THIERRY | European Patent Office | 2022

    Free access