Aircraft jet engine pylon suspension attachment
US7971825B2 · kind B2 · utility
14Cited by
8References
11Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 22, 2006 |
| Grant date | Jul 5, 2011 |
| Priority date | — |
| Expiry date | Jan 17, 2027 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/18
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The invention relates to a turbojet suspension pylon for an aircraft, the pylon being provided with a rigid structure (10) comprising a longitudinal central box (22). According to the invention, the rigid structure also comprises two lateral boxes (24a, 24b) fixed to a forward part of said central box (22), the pylon also comprising a first (6a) and a second (6b) engine forward suspension designed to resist forces applied along the longitudinal direction (X) of the pylon, these first and second suspensions being arranged on the two lateral boxes respectively.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.