Turbojet engine nacelle
US8845287B2 · kind B2 · utility
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6References
12Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 31, 2012 |
| Grant date | Sep 30, 2014 |
| Priority date | — |
| Expiry date | Dec 31, 2032 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D29/08
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A nacelle for a turbojet engine is provided that includes an air intake upstream from the turbojet engine, a middle section intended to surround a fan of the turbojet engine and its case, and a downstream section. The middle section is made from at least one aerostructure capable of ensuring external aerodynamic continuity of the nacelle, and the aerostructure is rigidly bound, so as to be able to be taken apart, to at least one surrounding fixed structure.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.