Multi-spar Wing Element Integrating Wet Dry Bays

The patent merges multiple separate spars into a single integrated multi-spar element that contains multiple internal bay spaces. This single element performs the function of multiple separate spars while reducing the total number of components, thereby decreasing device complexity and production cost while maintaining the ability to accommodate both wet and dry bays with their respective components.

The patent implements a nested structure where multiple bay spaces (wet bays and dry bays) are contained within a single multi-spar element. The internal bays are nested within the external boundaries of one integrated spar structure, allowing efficient space utilization and component accommodation without requiring additional external spars.

The patent combines multiple spar functions into a single manufactured element. The multi-spar element is produced as one integrated component through resin infusion molding, which maintains the structural separation of internal bays while eliminating the need to manufacture and assemble multiple separate spars, thereby reducing manufacturing cost and part count.

The single multi-spar element performs multiple functions that would traditionally require separate spars: it provides structural support, creates separation between wet and dry bays, and accommodates various mechanical and electrical components. This multi-functional design reduces the number of parts needed while maintaining structural integrity.

The patent segments the wing interior space into multiple distinct bays (wet bays for fuel storage and dry bays for component accommodation) within a single multi-spar element. This segmentation allows simultaneous optimization of fuel storage volume and component space by creating dedicated zones for each function without requiring additional external spars.

The patent nests multiple functional bays within the internal structure of a single multi-spar element. The wet bays and dry bays are nested within the external boundaries of one integrated spar, maximizing the utilization of available wing interior space for both fuel storage and component accommodation.