Air intake for aircraft nacelle, and propulsion assembly including such air intake
US8985506B2 · kind B2 · utility
3Cited by
11References
10Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jan 21, 2009 |
| Grant date | Mar 24, 2015 |
| Priority date | — |
| Expiry date | Jan 21, 2029 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2220/36
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The invention relates to an air intake for an aircraft nacelle that includes a shroud that can be mounted on the fan casing of a turbojet engine. The shroud is sized so as to define a circumferential gap relative to the casing. Punctual linking means between the shroud and the casing are discretely distributed at the periphery of the shroud.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.