Gas turbine engine with cooling air system
US10544740B2 · kind B2 · utility
0Cited by
11References
16Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Mar 15, 2016 |
| Grant date | Jan 28, 2020 |
| Priority date | — |
| Expiry date | Oct 19, 2037 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine including an engine core and a cooling air system is disclosed herein. The cooling air system is fluidly coupled between a compressor section of the engine core and a turbine section of the engine core to conduct pressurized air from the compressor section to the turbine section to cool components of the turbine section.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.