An anti-icing system (250) is disclosed. In various embodiments, the anti-icing system includes an inner duct (252) having a forward end configured to deliver a heated gas to a plenum (240) and an aft end spaced from the forward end; an outer duct (256) circumferentially encompassing at least a portion of the inner duct (252); and a forward seal system (280) disposed proximate the forward end, the forward seal system (280) including an aft attachment flange (282) configured for positioning adjacent an aft bulkhead face of a forward bulkhead (236), the inner duct (252) and the outer duct (256) being connected to the aft attachment flange (282), and a seal (285) configured for positioning adjacent a forward flange face of the aft attachment flange (282).


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    Title :

    INLET ANTI-ICE DOUBLE WALLED DUCT WITH SUPPLY LINE SEAL


    Additional title:

    DOPPELWANDIGER ANTI-EIS-EINLASSKANAL MIT VERSORGUNGSLEITUNGSABDICHTUNG
    CONDUIT D'ADMISSION ANTIGIVRE À DOUBLE PAROI AVEC JOINT DE LIGNE D'ALIMENTATION


    Contributors:

    Publication date :

    2022-01-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F16L PIPES , Rohre



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