Air guiding device and aircraft engine with air guiding device
US10309309B2 · kind B2 · utility
1Cited by
3References
17Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Sep 4, 2015 |
| Grant date | Jun 4, 2019 |
| Priority date | — |
| Expiry date | Jun 23, 2036 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
An air guiding device in an aircraft engine, comprising at least one connection device of a core engine shroud with an external wall of a bypass duct of the aircraft engine is provided. At least one first air inlet opening for inflowing air is connected to a connection device or is arranged inside the connection device.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.