Hybrid aircraft having rectifier with integrated protection
US11840148B2 · kind B2 · utility
Assignees
Inventors
Key dates
| Filing date | Feb 15, 2022 |
| Grant date | Dec 12, 2023 |
| Priority date | — |
| Expiry date | Feb 15, 2042 |
Classification
- Technology area (CPC H)Electricity
- CPC primaryH02J2310/44
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A system includes a first generator configured to output a first plurality of AC signals; a second generator configured to output a second plurality of AC signals; a first set of rectifiers configured to convert the first plurality of AC signals into a first plurality of DC signals for output onto a first DC bus, wherein each of the first set of rectifiers includes a respective contactor configured to de-couple a DC output of the respective rectifier from the first DC electrical bus; and a second set of rectifiers configured to convert the second plurality of AC signals into a second plurality of DC signals for output onto a second DC bus, wherein each of the second set of rectifiers includes a respective contactor configured to de-couple a DC output of the respective rectifier from the second DC bus.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.