Device for recovery of forces generated by an aircraft engine
US6648271B2 · kind B2 · utility
4Cited by
11References
5Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 7, 2002 |
| Grant date | Nov 18, 2003 |
| Priority date | — |
| Expiry date | Jun 7, 2022 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/402
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A device for recovering forces generated by an aircraft engine has an engine strut (10), capable of being fixed to a wing or a fuselage of an aircraft, and an attachment device (12) fixed to the engine strut (10) and on which the engine is mounted. An intermediate fitting (24) of large dimensions, capable of recovering exceptionally high forces is fixed to several strut fittings (30) independent from each other, for example by bolts (28), across a lower spar (14) of the engine strut (10).
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.