A fuel line coupling component (e.g., for aircraft fuel lines) allow for axial, rotational and radial displacements. The fuel line coupling component includes outer and inner tubular members with each having coaxially aligned pairs of coaxially sleeved tubular sections that are coaxially displaceable relative to one another. A pair of terminal end connectors includes a journalled connection assembly with the respective opposed distal ends of the outer and inner tubular members to thereby allow simultaneous rotational movements of the outer and inner tubular members about a longitudinal axis thereof and simultaneous radial displacements of outer an inner tubular members relative to a reference plane. C-clamps associated with fuel tank fittings and band clamps allow coupling of the fuel line coupling component to the fuel tank fittings and thereby fluid-connect aircraft fuel tanks (e.g., the aircraft main and auxiliary fuel tanks).


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    Title :

    DOUBLE WALLED FUEL LINE COUPLING COMPONENTS AND ASSEMBLIES CAPABLE OF MULTIPLE DEGREES OF DISPLACEMENT


    Additional title:

    DOPPELWANDIGE KRAFTSTOFFLEITUNGSKUPPLUNGSKOMPONENTEN UND ANORDNUNGEN MIT MEHREREN VERSCHIEBUNGSGRADEN
    COMPOSANTS ET ENSEMBLES DE COUPLAGE DE CONDUITE DE CARBURANT À DOUBLE PAROI POUVANT ÊTRE DÉPLACÉS DE MULTIPLES DEGRÉS



    Publication date :

    2025-02-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16L PIPES , Rohre / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02M Zuführen von Brennstoff-Luft-Gemischen oder deren Bestandteilen bei Brennkraftmaschinen allgemein , SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF



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