Mounting device for an aircraft engine comprising two thrust recovery rods with a double rear mechanical connection
US7607609B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Jun 27, 2007 |
| Grant date | Oct 27, 2009 |
| Priority date | — |
| Expiry date | Feb 14, 2028 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/404
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A mounting device for an aircraft engine includes a rigid structure and a device for mounting the engine on the rigid structure, the mounting device including a thrust load recovery device with two lateral thrust load recovery rods each having a rear end mounted on a crossbar of the recovery device with a first mechanical connection. At the rear end of each of the two rods, there is also provided a second mechanical connection with play between the rear end and a support fitting integral with the rigid structure. The first mechanical connection is implemented using a pin provided on the crossbar, passing through an orifice provided in the rear end of the rod.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.