Thermoplastic multi-grid overmolded/co-consolidated aircraft fuselage structure
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United States of America Patent
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Nov 1, 2022
Grant Date -
Apr 2, 2020
app pub date -
Sep 27, 2018
filing date -
Sep 27, 2018
priority date (Note) -
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Abstract
An aircraft structure and its method of construction avoids the inefficiencies involved in current methods of constructing the aircraft structure, reduces the manufacturing time required for constructing the aircraft structure and reduces the cost involved in constructing the aircraft structure. The aircraft structure and its method of construction is comprised of a geodesic or multi-grid framework of intersecting thermoplastic composite strips that are joined to an interior surface of a thermoplastic composite fuselage skin panel through overmolding/co-consolidation of the grid framework and the skin panel.
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