An aircraft wing (25) includes a rib (30) attached by a joint (39) to a tubular spar (28) that varies in cross sectional shape during flight. The joint (39) includes a ring (42) attached to the tubular spar (28), and pivot pins (40) connecting the ring (42) with the rib (30). The pivot pins (40) allow relative movement between the rib (30) and the tubular spar (28) as the tubular spar (28) varies in cross sectional shape. (Fig. 4)


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ATTACHMENT OF AIRCRAFT RIBS TO SPARS HAVING VARIABLE GEOMETRY


    Weitere Titelangaben:

    ANBRINGUNG VON FLUGZEUGRIPPEN AN HOLME MIT VARIABLER GEOMETRIE
    FIXATION DE NERVURES D'AÉRONEF POUR LONGERONS À GÉOMÉTRIE VARIABLE


    Beteiligte:

    Erscheinungsdatum :

    09.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Attachment of aircraft ribs to spars having variable geometry

    KRUSE JOHN SCOTT / FOGARTY JOHN HERSHEY | Europäisches Patentamt | 2016

    Freier Zugriff

    Influence of ribs on strength of spars

    Ballenstedt, L. | Engineering Index Backfile | 1923


    Wing with inflatable spars and rigid ribs

    Emerald Group Publishing | 1998



    Influence of Ribs on Strength of Spars

    Ballenstedt, L | NTRS | 1923