Engine nacelle
US10072511B2 · kind B2 · utility
1Cited by
19References
6Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Aug 28, 2015 |
| Grant date | Sep 11, 2018 |
| Priority date | — |
| Expiry date | Feb 23, 2036 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/10
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A nacelle for a gas turbine jet engine for an aircraft includes flow disruptors to provide boundary layer turbulence when the engine is exposed to air flow that is obtuse to direction of travel of the engine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.