The invention discloses a transversely assembled wing structure with the high aspect ratio and an assembly method of the wing structure. The wing structure comprises a front edge assembly, a wing beam assembly and a rear edge assembly, wherein the front edge assembly comprises a longitudinal front wall, a front edge wing rib group and a front edge skin; the front edge wing rib group comprises a plurality of front edge wing ribs which are longitudinally arranged in parallel; each front edge wing rib is fixedly connected to a longitudinal front wall; the front edge skin is connected to the periphery of the front edge wing rib group; the wing beam assembly comprises a longitudinal wing beam group, a reinforced wing rib group, an upper skin and a lower skin; the longitudinal wing beam group comprises a plurality of longitudinal wing beams which are transversely arranged in parallel; the reinforced wing rib group comprises a plurality of reinforced wing ribs which are longitudinally arranged in parallel; the reinforced wing rib group is fixedly connected to the longitudinal wing beam group; the upper skin is connected to the upper side of the reinforced wing rib group; the lower skin is connected to the lower side of the reinforced wing rib group; and the rear edge assembly comprises a longitudinal rear wall, a rear edge wing rib group and a rear edge skin. The transversely assembled wing structure has the excellent mechanical property, and is high in disassembling efficiency, small in space occupied for transportation, and convenient to transport.
Transversely assembled wing structure with high aspect ratio and assembly method of wing structure
2015-04-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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