Propulsion assembly for aircraft
US8534597B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Aug 28, 2008 |
| Grant date | Sep 17, 2013 |
| Priority date | — |
| Expiry date | Jun 19, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/404
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The invention relates to a propulsion assembly for an aircraft, that comprises: a turbojet engine (1) including a fan casing (3) and an engine casing (5); a pylon for holding said turbojet engine (1); and a device for suspending said turbojet engine under the pylon, that comprises two front suspension connecting rods (9), two rear suspension connecting rods (11), and a thrust acceleration connecting rod (15) extending between the front portion (17) of said engine casing (5) and the pylon in a plane containing the axis (A) of said turbojet engine (1). An additional connecting rod (19) extends between said fan casing (3) and said pylon in a direction substantially parallel to that of the axis (A) of said turbojet engine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.