Engine assembly for aircraft
US7445179B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Sep 27, 2006 |
| Grant date | Nov 4, 2008 |
| Priority date | — |
| Expiry date | May 3, 2027 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/406
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The invention relates to an engine suspension pylon for an aircraft including a rigid structure provided with a box (24), this pylon also including an engine aft attachment (8) provided with an attachment body (38), and a thrust resistance device (9) generated by the engine. The rigid structure according to the invention includes an offset rib (35) for the attachment body (38), this rib (35) being mounted fixed on the box (24) between the box and the engine (2) and carrying the attachment body. Furthermore, the device (9) includes a thrust resistance spar (9b) of which the forward end is mounted fixed on the rib (35), and the aft end is mounted fixed on the box.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.