Air cooler system for gas turbine engines
US10072577B2 · kind B2 · utility
2Cited by
28References
14Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 15, 2016 |
| Grant date | Sep 11, 2018 |
| Priority date | — |
| Expiry date | Mar 23, 2037 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A buffer air cooler system for gas turbine engines disposed in a bypass duct of the engine, includes a housing for containing the buffer air cooler therein and an inlet portion attached to the housing. In one embodiment, the inlet portion has a double-skin configuration in at least one region of a top, bottom and sides of the inlet portion.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.