System and method for stabilizing transcritical air-to-fuel heat exchange
US10890114B2 · kind B2 · utility
1Cited by
1References
33Claims
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Key dates
| Filing date | Mar 30, 2017 |
| Grant date | Jan 12, 2021 |
| Priority date | — |
| Expiry date | Jan 25, 2039 |
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 devices, systems, and methods for design and operation of stabilizing heat exchangers for gas turbine engines in consideration of near supercritical fuel flow conditions.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.