Fuselage sub-floor structure with aircraft components having corrugated C-channel
AssigneeCivil Aviation University of China
InventorsHaolei Mou, Xingyan Liu, Jiang Xie, Zhenyu Feng
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AssigneeCivil Aviation University of China
InventorsHaolei Mou, Xingyan Liu, Jiang Xie, Zhenyu Feng
Estimating the term…
An aircraft fuselage sub-floor structure with an aircraft column component includes an upper fuselage frame, a lower curved fuselage frame, and a corrugated corrugated C-channel component. The upper fuselage frame is integrated with a cargo floor crossbeam, and the upper fuselage frame connects with the lower curved fuselage frame through a splice plate. The lower curved fuselage frame is divided into left and right sections at the bottom, and is strengthened by a doubler at the bottom of the docking. The corrugated C-channel includes an intermediate corrugated section and a straight section arranged at both ends of the intermediate corrugated section. The straight section of the corrugated C-channel is connected to the cargo floor crossbeam and the upper curved fuselage frame through the upper and lower stanchion fitting respectively. The upper and lower stanchion fitting flanges are connected to the flanges on both sides of the straight section.
An aircraft column component, comprising:
Dependencies are inferred from the claim text.