Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle
US8757541B2 · kind B2 · utility
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19References
5Claims
0Family size
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Key dates
| Filing date | Jun 3, 2009 |
| Grant date | Jun 24, 2014 |
| Priority date | — |
| Expiry date | Sep 24, 2030 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D2033/0286
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft nacelle comprising a power plant having a pipe with an aerodynamic surface, an air intake having an inside pipe with an aerodynamic surface, and an annular support of at least one measuring device having an aerodynamic surface, wherein the annular support is removably-inserted between the power plant and the air intake. In particular, the annular support is inserted downstream of the air intake and upstream of the power plant in a direction of flow of the stream of air, in such a way as to ensure continuity of the aerodynamic surfaces.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.