The invention relates to an aircraft having two main landing gears and a main landing gear bay (34) configured to accommodate the two main landing gears in a collapsed state on both sides of a vertical midline plane, the main landing gear bay (34) comprising a rear transverse wall (36), a front transverse wall (38) and a bottom wall (40) substantially perpendicular to the rear transverse wall (36) and the front transverse wall (38), characterized in that the main landing gear compartment (34) comprises at least one strut (56, 58) connecting the rear transverse wall (36) or the front transverse wall (38) and the bottom wall (40) and positioned substantially in a vertical midline plane.
本发明涉及一种具有两个主起落架以及主起落架舱(34)的飞行器,该主起落架舱被构造为能够在竖直中线平面的两侧容纳处于收缩状态的两个主起落架,该主起落架舱(34)包括后横向壁(36)、前横向壁(38)以及基本垂直于后横向壁(36)和前横向壁(38)的底壁(40),其特征在于,该主起落架舱(34)包括至少一个支柱(56,58),其连接后横向壁(36)或前横向壁(38)和底壁(40),并大致定位于竖直中线平面中。
Aircraft comprising reinforced main landing gear bay
包括加强的主起落架舱的飞行器
2022-07-19
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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