Stiffener for an aircraft assembly
US11312467B2 · kind B2 · utility
1Cited by
3References
19Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Dec 20, 2018 |
| Grant date | Apr 26, 2022 |
| Priority date | — |
| Expiry date | Apr 15, 2040 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2001/0072
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A stiffener for an aircraft assembly is disclosed. The stiffener provides structural stability to the aircraft assembly. The stiffener has a first stiffener part having a planar web portion and a second stiffener part arranged with the first stiffener part. The second stiffener part includes a corrugated web portion having a corrugation. The present application also relates to an aircraft assembly, a fuselage for an aircraft, an aircraft and a method of forming a stiffener for an aircraft assembly.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.