Electrical architecture for an aircraft, aircraft comprising the architecture and method for operating the architecture
US11509245B2 · kind B2 · utility
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10Claims
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Key dates
| Filing date | Jun 20, 2019 |
| Grant date | Nov 22, 2022 |
| Priority date | — |
| Expiry date | Jun 26, 2041 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/80
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An architecture for an aircraft comprises two air-conditioning systems, two converters, each intended to supply one of the air-conditioning systems, and at least one first electric machine which starts up a first main engine of the aircraft. The electrical architecture is configured such that the two converters can together supply the first electric machine. A method of operating the architecture is also provided.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.