A structural assembly of an aircraft has a fastener 112 extending into first and second structural members 102, 108. A washer 120 is disposed between the fastener 112 and one of the structural members 102, 108 to electrically insulate the fastener 112 and the structural members 102, 108. The washer 120 has a core of reinforcement fibres supported in a thermoplastic matrix material. Electrically-insulating outer layers of glass fibres overlay the core.


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    Title :

    Aircraft electrical isolation component and method of manufacturing electrical isolation component


    Contributors:

    Publication date :

    2018-08-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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



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