Gas turbine engine with air/fuel heat exchanger
US9771867B2 · kind B2 · utility
46Cited by
51References
19Claims
0Family size
Assignees
Inventors
Key dates
| Filing date | Jun 30, 2014 |
| Grant date | Sep 26, 2017 |
| Priority date | — |
| Expiry date | Dec 5, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldThermal processes and apparatus
- WIPO sectorMechanical engineering
Abstract
One embodiment of the present invention is a unique aircraft propulsion gas turbine engine. Another embodiment is a unique gas turbine engine. Another embodiment is a unique gas turbine engine. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines with heat exchange systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.