Engine nacelle for an aircraft
US10974813B2 · kind B2 · utility
0Cited by
12References
17Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jan 8, 2018 |
| Grant date | Apr 13, 2021 |
| Priority date | — |
| Expiry date | Aug 8, 2038 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An engine nacelle is provided for an aircraft. The engine nacelle comprises: an inlet for receiving an air flow to generate a thrust force for the aircraft; a lip portion positioned at the inlet and surrounding the inlet; and at least one strake provided on a surface of the engine nacelle.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.