Gas turbine engine and fuel cell assembly
US12270340B2 · kind B2 · utility
0Cited by
104References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jan 4, 2024 |
| Grant date | Apr 8, 2025 |
| Priority date | — |
| Expiry date | Jan 4, 2044 |
Classification
- Technology area (CPC H)Electricity
- CPC primaryH01M8/0618
- WIPO fieldElectrical machinery, apparatus, energy
- WIPO sectorElectrical engineering
Abstract
A gas turbine engine is provided. The gas turbine engine includes a turbomachine having a compressor section, a combustor, and a turbine section arranged in serial flow order, the turbomachine further including an outer casing and, during operation of the gas turbine engine, an exhaust gas flow from the turbine section; and a fuel cell assembly positioned within the outer casing of the turbomachine, the fuel cell assembly having a fuel cell defining an inlet positioned to receive a portion of the exhaust gas flow, an outlet positioned to provide output products directly to the exhaust gas flow, or both.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.