Engine pylon for the suspension of a turbo engine under an aircraft wing
US8336813B2 · kind B2 · utility
6Cited by
5References
7Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Aug 31, 2009 |
| Grant date | Dec 25, 2012 |
| Priority date | — |
| Expiry date | Jan 5, 2031 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C7/02
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
According to the invention, the engine pylon for the suspension of a turbo engine under an aircraft wing is such that the trailing edge of the rear lower part of the engine pylon is shifted toward the root of the wing.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.