RIGID OPEN COMPOSITE PANEL
Number of patents in Portfolio can not be more than 2000
United States of America
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N/A
Issued Date -
Jan 9, 2025
app pub date -
Nov 16, 2022
filing date -
Nov 16, 2022
priority date (Note) -
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status (Latency Note)
Importance
Abstract
An open composite panel for an aircraft includes a composite skin having an inner face and an outer face, and a plurality of stiffening ribs, each rib extending over the inner face of the skin in a respective direction of extension and projecting from the inner face to a top that is opposite said inner face. The plurality of ribs includes at least one reinforced rib, each reinforced rib having at least one elongate stiffening portion extending along the top of the reinforced rib, said stiffening portion including fibers extending substantially in the direction of extension of the reinforced rib.
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