Structural component and method for producing a structural component
US9988136B2 · kind B2 · utility
109Cited by
9References
16Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Oct 29, 2015 |
| Grant date | Jun 5, 2018 |
| Priority date | — |
| Expiry date | Jan 22, 2036 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02P10/25
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A structural component for reinforcing the fuselage of an aircraft or spacecraft is integrally formed and segmented into surface-like stiffening sections, whereby at least one stiffening section is formed as a rigid mesh section, and at least one stiffening section is formed as a solid section.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.