Provided are a frame assembly for a rear section of an aircraft and a rear section of an aircraft. The frame assembly comprises at least one frame (2) having a plane of symmetry (4), wherein the frameassembly also comprises at least one supporting element (3) having two ends (3'), wherein each one of the ends (3') is attached to said at least one frame (2) at different sides of the plane of symmetry (4).It permits a more effective transfer of loads coming from the vertical tail plane of the aircraft to the fuselage.
一种用于飞行器的后部部段的框架组件和飞行器的后部部段,所述框架组件包括具有对称平面(4)的至少一个框架(2),其中,所述框架组件还包括具有两个端部(3’)的至少一个支撑元件(3),其中所述端部(3’)中的每一个端部在所述对称平面(4)的不同侧附接至所述至少一个框架(2)。所述框架组件允许将来自飞行器的垂直尾翼的载荷更有效地传递至机身。
Frame assembly for rear section of aircraft and rear section of aircraft
用于飞行器的后部部段的框架组件和飞行器的后部部段
26.05.2020
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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