An anti-icing system is disclosed. In various embodiments, the anti-icing system includes an inner duct having a first end configured to deliver heated gas to a plenum and a second end spaced from the first end; an outer duct circumferentially encompassing at least a portion of the inner duct; and a seal system disposed proximate the second end, the seal system including a first annular seal having a radially inner end positioned proximate a flange disposed on the inner duct.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Anti-ice double walled duct system


    Beteiligte:
    KROEGER DANIEL (Autor:in) / RAMLAOUI JIHAD (Autor:in) / RATAJAC ALEKSANDAR (Autor:in)

    Erscheinungsdatum :

    2022-01-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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



    ANTI-ICE DOUBLE WALLED DUCT SYSTEM

    KROEGER DANIEL / RAMLAOUI JIHAD / RATAJAC ALEKSANDAR | Europäisches Patentamt | 2024

    Freier Zugriff

    ANTI-ICE DOUBLE WALLED DUCT SYSTEM

    KROEGER DANIEL / RAMLAOUI JIHAD / RATAJAC ALEKSANDAR | Europäisches Patentamt | 2020

    Freier Zugriff

    INLET ANTI-ICE DOUBLE WALLED DUCT WITH SUPPLY LINE SEAL

    KROEGER DANIEL / GRAILY BAHRAM B | Europäisches Patentamt | 2022

    Freier Zugriff

    Double-duct manned aircraft

    WEN HONGJUN | Europäisches Patentamt | 2020

    Freier Zugriff

    Double-duct tilt aircraft

    XU JINPENG | Europäisches Patentamt | 2015

    Freier Zugriff