An aircraft, a center wing box assembly for an aircraft, and a spanwise beam section for a center wing box assembly that includes a segmented structural configuration with an optimized access hole to accommodate user access into an interior space of the center wing box for purposes of assembly and maintenance. The center wing box assembly includes a first spanwise beam section, a second spanwise beam section, spaced from the first spanwise beam section, and a plurality of chord members serving as load-bearing structural reinforcement members for the first spanwise beam section and the second spanwise beam section. The chord members extend across the space between the first spanwise beam section and the second spanwise beam section to connect the first spanwise beam section and the second spanwise beam section in a manner which defines an access hole at the interior space.
SEGMENTED SPANWISE BEAM FOR ENHANCED CENTER WING BOX ACCESS
2024-05-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
SEGMENTED SPANWISE BEAM FOR ENHANCED CENTER WING BOX ACCESS
European Patent Office | 2024
|Segmented wing test technique for obtaining spanwise load distributions
Engineering Index Backfile | 1967
|NTIS | 2018
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