Electric architecture for a hybrid thermal/electric propulsion aircraft and twin-engined aircraft comprising such an architecture
US12097965B2 · kind B2 · utility
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20Claims
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Key dates
| Filing date | Nov 12, 2020 |
| Grant date | Sep 24, 2024 |
| Priority date | — |
| Expiry date | Feb 24, 2041 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An electric architecture for a twin-engined, hybrid thermal/electric propulsion aircraft and, for each turboshaft which includes a high-voltage DC propulsive electric distribution network, a non-propulsive electric distribution network which is connected to loads of the aircraft, and an electric distribution network which is connected to loads of an electrified control system of the turboshaft engine, and wherein power supply sources are shared for these different networks.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.