To provide an interface between an outer skin and a panel of a stabilizer and wing of an aircraft, which achieves at least some of low weight, low cost, easy handling and durability.SOLUTION: A wing or stabilizer of an aircraft comprises a box portion comprising at least one spar and an outer skin (130) coupled to the at least one spar. The wing or stabilizer also comprises at least one panel (134) comprising an outer face-sheet (150) and an inner face-sheet (152). In a fore-aft direction, the outer face-sheet (150) terminates at an outer free edge (180). In the fore-aft direction, the inner face-sheet (152) terminates at an inner free edge (158). The at least one panel (134) also includes a core (178) sandwiched between the outer face-sheet (150) and the inner face-sheet (152). The inner face-sheet (152) comprises a cantilevered portion (154) defining the inner free edge (158) and fastened to the outer skin (130) of the box portion.SELECTED DRAWING: Figure 4

    【課題】重量、コスト、取り扱いの容易さ、耐久性の少なくともいくつかを克服する航空機の安定板及び翼の外板パネル境界面を提供する。【解決手段】航空機の翼又は安定板は、少なくとも1つのスパー及び少なくとも1つのスパーに連結された外板(130)を含むボックス部分を含む。翼又は安定板はまた、外面シート(150)及び内面シート(152)を含む少なくとも1つのパネル(134)を含む。前後方向において、外面シート(150)は、外側の自由端(180)で終端する。前後方向において、内面シート(152)は、内側の自由端(158)で終端する。少なくとも1つのパネル(134)はまた、外面シート(150)と内面シート(152)との間に挟まれたコア(178)を含む。内面シート(152)は、片持ち型部分(154)を含み、内側の自由端(158)を画定し、ボックス部分の外板(130)に固定される。【選択図】図4


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    Title :

    SKIN-PANEL INTERFACE OF AIRCRAFT


    Additional title:

    航空機の外板パネル境界面


    Contributors:

    Publication date :

    2019-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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