PROBLEM TO BE SOLVED: To provide aircraft wings that are stiffened using non-integral stiffeners that are relatively small and easy to manufacture and/or use, where the wings may include composite and/or carbon fiber reinforced plastic (CFRP) and realize light weights and low costs.SOLUTION: An aircraft wing 104 has: a first panel 106; a second panel 108; ribs 202 coupled between the first and second panels; and stiffeners 204 coupled between the ribs in a spanwise direction and to the first panel. The couplings between the stiffeners and the first panel deter axial loads from being received by the stiffeners. The stiffeners increase a compressional stability of the first panel. The couplings between the stiffeners and the first panel are indirect couplings formed via clips. The couplings formed via the clips deter the axial loads from being received by the stiffeners while increasing the compressional stability of the first panel.SELECTED DRAWING: Figure 2

    【課題】比較的小型で製造及び/又は使用が容易な非一体型補強材を使用して補強される、複合材及び/又は炭素繊維強化プラスチック(CFRP)を含みうる、低コスト軽量な航空機翼を提供する【解決手段】航空機翼104は第1のパネル106、第2のパネル108、第1のパネルと第2のパネルとの間に連結されたリブ202、並びに、リブ間に翼長方向に連結され且つ第1のパネルに連結された補強材204を有する。補強材と第1のパネルとの間の連結は軸荷重が補強材によって受容されるのを防ぎ、補強材は第1のパネルの圧縮安定性を高め、補強材と第1のパネルとの間の連結はクリップによって形成された間接的な結合で、クリップによって形成された連結は軸荷重が補強材によって受容されるのを防ぎ、一方で第1のパネルの圧縮安定性を高める。【選択図】図2


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    Title :

    AIRCRAFT WINGS AND AIRCRAFT INCLUDING THOSE AIRCRAFT WINGS


    Additional title:

    航空機翼及び当該航空機翼を含む航空機


    Contributors:

    Publication date :

    2018-05-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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