Method for fixing an engine strut to an airplane wing
US7963479B2 · kind B2 · utility
10Cited by
2References
9Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Nov 17, 2005 |
| Grant date | Jun 21, 2011 |
| Priority date | — |
| Expiry date | May 29, 2026 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/404
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The inventive fixing system comprises a front attachment (6), a rear attachment (7) and an intermediate attachment (8) connecting a strut (1) to a wing (2), wherein the lower fitting (17) of the rear attachment (7) is fixedly connected to the transversal rear face (1 G) of said strut on the extension thereof and said lower fitting (17) is substantially in flush with the top face of the strut.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.