A high lift component includes at least one intermediate seal on at least one lateral surface, wherein the intermediate seal includes at least one hollow body made of an elastic material, which hollow body includes a fluid inlet that is connectable to a fluid source. A gap between two high lift components, which gap is subjected to dynamic changes in geometry, can be flexibly sealed in this manner.


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    Title :

    HIGH LIFT COMPONENT FOR AN AIRCRAFT, HIGH LIFT SYSTEM, METHOD FOR ADJUSTING THE HIGH LIFT CHARACTERISTICS OF AN AIRCRAFT AND AIRCRAFT


    Additional title:

    HOCHAUFTRIEBSKOMPONENTE FÜR EIN FLUGZEUG, HOCHAUFTREIBSSYSTEM, VERFAHREN ZUM ANPASSEN DER HOCHAUFTRIEBSEIGENSCHAFTEN EINES FLUGZEUGES UND FLUGZEUG
    ÉLÉMENT HYPERSUSTENTATEUR POUR AVION, SYSTÈME HYPERSUSTENTATEUR, PROCÉDÉ DE RÉGLAGE DES CARACTÉRISTIQUES D'HYPERSUSTENTATION D'UN AVION, ET AVION


    Contributors:

    Publication date :

    2018-11-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge




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