The invention relates to a tolerance compensation subassembly (24) in the form of a tolerance compensation element (26) or a tolerance compensation region in order to improve the production, maintenance and repair of aircraft. The tolerance compensation subassembly (24) contains an actuator (54) which is formed from an electro-active polymer so that the tolerance compensation subassembly (24) is electrically switchable between a fixed state and a non-fixed state. As a result, automation of the assembly of aircraft components on each other can be enabled or facilitated.


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    Title :

    TOLERANCE COMPENSATION SUBASSEMBLY, AIRCRAFT COMPONENT PROVIDED THEREWITH AND AIRCRAFT


    Additional title:

    TOLERANZAUSGLEICHSANORDNUNG, FLUGZEUGBAUTEIL DAMIT UND FLUGZEUG
    SOUS-ENSEMBLE DE COMPENSATION DE TOLÉRANCE, COMPOSANT D'AÉRONEF EN ÉTANT ÉQUIPÉ ET AÉRONEF


    Contributors:

    Publication date :

    2022-09-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H10N / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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