Assembly of an inner fixed structure of a turbojet engine nacelle and of a thermal protection
US10001064B2 · kind B2 · utility
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2References
5Claims
0Family size
Assignee
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Key dates
| Filing date | Apr 24, 2017 |
| Grant date | Jun 19, 2018 |
| Priority date | — |
| Expiry date | Apr 24, 2037 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The present disclosure relates to an assembly of an inner fixed structure of a turbojet engine nacelle and of a thermal protection, said structure including an inner face, on which the thermal protection is added, and an outer face constituting a portion of the inner surface of a cold flow path, the assembly including at least one channel put in fluid communication the inner face and the outer face of the structure.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.