A winglet comprising first and second covers 20, (22, figure 2) and a mid spar 28 between front and rear spars 24, 26. Each spar is joined to the first and second covers. The mid spar has an I-shaped cross-section comprising a mid spar web (29, figure 5) a first pair of mid spar caps (29a, 30a), joining the mid spar to the first cover, and a second pair of mid spar caps (29b, 30b) joining the mid spar to the second cover. The mid spar curves along all or part of its length. A winglet cover assembly is disclosed with a cover and a spar formed from fibre reinforced composite material. The cover and spar(s) may be provided by co-infusing preforms with a matrix material and bonded by co-curing the matrix material. The spar and/or mid spar may follow a three dimensional curvature, twisting along its length.


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    Titel :

    Winglet and winglet cover assembly


    Beteiligte:
    THOMAS BARNETT (Autor:in) / ANDREW SCAIFE (Autor:in) / LEE PROUDLER (Autor:in)

    Erscheinungsdatum :

    2022-02-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / 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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