The invention provides an aircraft wing box assembly comprising: a wing box having an upper cover, a lower cover, and a pair of spars; and a plurality of ribs in the wing box. The ribs divide the wing box into a plurality of compartments. The fuel tank is located in a first of the compartments. One of the spars includes a spar aperture configured to enable a fuel tank to be removed from a first of the compartments through the spar aperture.
本发明提供了一种飞行器机翼盒组件,该飞行器机翼盒组件包括:机翼盒,该机翼盒具有上覆盖件、下覆盖件和一对翼梁;位于机翼盒中的多个肋部。肋部将机翼盒划分为多个隔间。燃料箱位于隔间中的第一隔间中。翼梁中的一个翼梁包括翼梁孔,该翼梁孔构造成使燃料箱能够穿过翼梁孔从隔间中的第一隔间中移除。
Wing box with removable fuel tank
具有可移除燃料箱的机翼盒
2022-08-30
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |