According to the invention a vented leading-edge assembly is provided, the assembly (10) comprising: a slat (12) comprising a bay (14) and a top skin (16) delimiting a portion of the bay (14); a spar(18) being arranged in the slat (12), the spar (18) dividing the bay (14) in a front bay (20) and an aft bay (22); and a plurality of channel sidewalls (24) being arranged between the top skin (16) and the spar (18), the plurality of channel sidewalls (24) defining a plurality of channels (26) between the front bay (20) and the aft bay (22), wherein at least a portion (30) of the spar (18) defineslower channel walls (28) for the plurality of channels (26). Thus, the invention provides an improved leading-edge assembly (10).

    根据本发明,提供了一种通气式前缘组件,所述组件(10)包括:缝翼(12),所述缝翼包括隔间(14)和界定所述隔间(14)的一部分的顶部蒙皮(16);翼梁(18),所述翼梁布置在所述缝翼(12)中,所述翼梁(18)将所述隔间(14)划分为前隔间(20)和后隔间(22);以及多个通道侧壁(24),所述多个通道侧壁布置在所述顶部蒙皮(16)与所述翼梁(18)之间,所述多个通道侧壁(24)限定了所述前隔间(20)与所述后隔间(22)之间的多个通道(26),其中,所述翼梁(18)的至少一部分(30)限定了所述多个通道(26)的下部通道壁(28)。因此,本发明提供了一种改进的前缘组件(10)。


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    Titel :

    Vented leading-edge assembly and method for manufacturing a vented leading-edge assembly


    Weitere Titelangaben:

    通气式前缘组件和用于制造通气式前缘组件的方法


    Beteiligte:
    BENSMANN STEFAN (Autor:in) / ERBAN MARCUS (Autor:in)

    Erscheinungsdatum :

    01.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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