The invention relates to an aircraft tail part comprising: a vertical tail; -a rear fuselage section attached to the vertical tail and comprising a skin and an internal reinforcement member; -a horizontal tail comprising two lateral torsion boxes and a frame structure located between the two lateral torsion boxes, the frame structure comprising a front spar, a rear spar and two ribs extending between the front spar and the rear spar, and each rib being adjacent to the lateral torsion box. The frame structure surrounds a part of the vertical tail in the wingspan direction of the vertical tail. The aircraft tail portion includes an attachment assembly that attaches the frame structure to the rear fuselage section, the attachment assembly extending across the skin and between an internal reinforcement member of the rear fuselage section and the frame structure.
一种飞行器尾翼部包括:‑垂直尾翼;‑后机身部段,所述后机身部段附接到所述垂直尾翼并且包括蒙皮和内部加强构件;‑水平尾翼,所述水平尾翼包括两个侧向抗扭箱以及位于所述两个侧向抗扭箱之间的框架结构,所述框架结构包括前翼梁、后翼梁以及在所述前翼梁与所述后翼梁之间延伸的两个肋,并且每个肋邻近侧向抗扭箱。所述框架结构沿着所述垂直尾翼的翼展方向包围所述垂直尾翼的一部分。所述飞行器尾翼部包括附接组件,所述附接组件将所述框架结构附接到所述后机身部段,所述附接组件跨过所述蒙皮并且在所述后机身部段的内部加强构件与所述框架结构之间延伸。
Aircraft empennage with horizontal stabilizers connected at root of vertical stabilizers
带有在垂直安定面根部处相接的水平安定面的飞行器尾翼部
2022-08-26
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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