An aircraft structure (10) and its method of construction avoids the inefficiencies involved in current methods of constructing the aircraft structure (10), reduces the 5 manufacturing time required for constructing the aircraft structure (10) and reduces the cost involved in constructing the aircraft structure (10). The aircraft structure (10) and its method of construction is comprised of a geodesic or multi-grid framework (16) of intersecting thermoplastic composite strips (22) that are joined to an interior surface (24) of a thermoplastic composite fuselage skin panel (18) through overmolding/co 10 consolidation of the grid framework (16) and the skin panel (18). 22 58 9 2 ,-3 -2 32-, 76,, 72-, (/92925384 92 '-66 92 48,-- -- . 92 -68 92 - -96 64--' ,2-- 62--'73 8-' 46 7~42 92 92 56
Thermoplastic multi-grid overmolded aircraft fuselage structure
2020-04-16
Patent
Elektronische Ressource
Englisch
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