Structural nacelle
US8739552B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Jun 11, 2007 |
| Grant date | Jun 3, 2014 |
| Priority date | — |
| Expiry date | Feb 19, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/18
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The present invention relates, on the one hand, to a nacelle (1) for a double flow turboreactor (2) comprising a front air intake section (5), a median section (6) intended for surrounding a fan (3) of the turboreactor and a rear section (7), said rear section having an internal structure (7b) intended for serving as a housing to a rear portion of the turboreactor, characterized in that the internal structure possesses attachment means suitable for enabling the nacelle to be fastened to a pylon (12) intended to be connected to a fixed structure (13) of an aeroplane on at least one portion of said internal structure, and on the other hand, to a propellant assembly and to an aircraft provided with such a nacelle.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.