A de-icing assembly for a surface of an aircraft includes: a carcass (38) with a first layer, a second layer, and a carcass centerline and a plurality of seams (42) sewn into the carcass (38), wherein the plurality of seams (42) join the first and second layers of the carcass (38) together. The assembly includes a plurality of inflation passages (52) formed by the plurality of seams (42) and disposed between the first and second layers of the carcass (38). The system also includes a manifold fluidly connected to and disposed beneath the carcass (38), the manifold comprising a width and a manifold centerline oriented approximately perpendicular or parallel to the carcass centerline. The seams (42) are sown by a stitchline formed of carbon nanotube yarn.


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    Titel :

    CARBON NANOTUBE YARN FOR PNEUMATIC DE-ICER STITCHING


    Weitere Titelangaben:

    KOHLENSTOFFNANORÖHRCHENGARN FÜR PNEUMATISCHE ENTEISUNGSNAHT
    FIL EN NANOTUBES DE CARBONE POUR L'ASSEMBLAGE D'UN DÉGIVREUR PNEUMATIQUE


    Beteiligte:
    SLANE CASEY (Autor:in) / WAINA DANIEL (Autor:in) / BOTURA GALDEMIR CEZAR (Autor:in)

    Erscheinungsdatum :

    09.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    CARBON NANOTUBE YARN FOR PNEUMATIC DE-ICER STITCHING

    SLANE CASEY / WAINA DANIEL / BOTURA GALDEMIR CEZAR | Europäisches Patentamt | 2022

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    Carbon nanotube yarn for pneumatic de-icer stitching

    SLANE CASEY / WAINA DANIEL / BOTURA GALDEMIR CEZAR | Europäisches Patentamt | 2024

    Freier Zugriff

    Pneumatic de-icer

    Gulick, J.E. | Engineering Index Backfile | 1944


    THE PNEUMATIC DE-ICER

    Gulick, J. E. | SAE Technical Papers | 1944


    ELECTRO-PNEUMATIC DE-ICER

    WIEGERS ROBERT GLYNN / SCHROEDER CRISTOPHER ROBERT | Europäisches Patentamt | 2018

    Freier Zugriff