Heat exchanger inlet vane assemblies with improved mixing trailing edge features
US12215621B1 · kind B1 · utility
0Cited by
13References
20Claims
0Family size
Assignee
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Key dates
| Filing date | Jul 31, 2023 |
| Grant date | Feb 4, 2025 |
| Priority date | — |
| Expiry date | Jul 31, 2043 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/213
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A gas turbine engine includes a heat exchanger and an inlet shroud. The heat exchanger is configured to transfer heat. The inlet shroud is configured to be coupled with the heat exchanger upstream of the heat exchanger.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.