Gas turbine engine with intercooling turbine section and intercooling turbine section bypass
US9341121B2 · kind B2 · utility
21Cited by
1References
30Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 12, 2014 |
| Grant date | May 17, 2016 |
| Priority date | — |
| Expiry date | Dec 12, 2034 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine includes an intercooling turbine section to selectively cool the core flow. An intercooling turbine section bypass is also included to selectively bypass at least a portion of a core flow through an intercooling turbine section bypass path around the intercooling turbine section.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.