Fuselage assembly for an aircraft
US10875619B2 · kind B2 · utility
0Cited by
4References
15Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Mar 26, 2019 |
| Grant date | Dec 29, 2020 |
| Priority date | — |
| Expiry date | Mar 26, 2039 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D2013/0625
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A fuselage assembly for an aircraft including a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.