Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel
US8006931B2 · kind B2 · utility
1Cited by
4References
7Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Mar 28, 2007 |
| Grant date | Aug 30, 2011 |
| Priority date | — |
| Expiry date | Sep 11, 2028 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C7/02
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft wing arrangement including a wing and at least one strut for attaching the aircraft engine suspended under the wing and including a front zone situated projecting towards the front with respect to a leading edge of the wing. The front zone includes a lateral projection delimiting a lateral air flow channel while being projected towards a proximal end of the wing.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.