Beaded composite structural web
US12214857B2 · kind B2 · utility
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1References
6Claims
0Family size
Assignee
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Key dates
| Filing date | Mar 22, 2023 |
| Grant date | Feb 4, 2025 |
| Priority date | — |
| Expiry date | Mar 22, 2043 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2001/0072
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.