The invention relates to the technical field of aircraft floors, and provides an aircraft composite material floor structure and a manufacturing method, and the aircraft composite material floor structure comprises a first panel; the core material is arranged at the bottom of the first panel; the second panel is arranged on one side, far away from the first panel, of the core material; the pre-embedded lining penetrates through the core material, one end of the pre-embedded lining is connected with the first panel, the other end of the pre-embedded lining is connected with the second panel, and the pre-embedded lining is used for fixing the floor structure. According to the aircraft composite material floor structure and the manufacturing method, the core material is arranged at the bottom of the first panel, the second panel is arranged on the side, away from the first panel, of the core material, the overall strength and rigidity of the floor structure are higher through arrangement of the core material, and consumed fuel is reduced during flight; in addition, due to the arrangement of the embedded linings, it can be guaranteed that the floor structure is fixed conveniently.
本发明涉及飞机地板技术领域,提供一种飞机复合材料地板结构及制作方法,其中,飞机复合材料地板结构包括第一面板;芯材,设置于所述第一面板的底部;第二面板,设置于所述芯材远离所述第一面板的一侧;预埋衬套,贯穿所述芯材,且所述预埋衬套的一端与所述第一面板连接,另一端与所述第二面板连接,所述预埋衬套用于固定所述地板结构。本发明提供的飞机复合材料地板结构及制作方法,通过芯材设置于第一面板的底部,第二面板设置于芯材远离第一面板的一侧,芯材的设置使得地板结构的整体强度和刚度更高,在飞行时减少所消耗的燃料;而且,预埋衬套的设置,能够保证便于固定地板结构。
Airplane composite material floor structure and manufacturing method
飞机复合材料地板结构及制作方法
26.01.2024
Patent
Elektronische Ressource
Chinesisch
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