Power system architecture for aircraft with electrical actuation
US10784701B2 · kind B2 · utility
3Cited by
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20Claims
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Key dates
| Filing date | Dec 7, 2017 |
| Grant date | Sep 22, 2020 |
| Priority date | — |
| Expiry date | May 29, 2038 |
Classification
- Technology area (CPC H)Electricity
- CPC primaryH02J2310/44
- WIPO fieldElectrical machinery, apparatus, energy
- WIPO sectorElectrical engineering
Abstract
An electrical power system for regenerative loads may include a DC bus and an electrical actuator load, where back-driving the electrical actuator load generates regenerative electrical energy, and where the electrical actuator load is configured to transmit the regenerative electrical energy to the DC bus. The system may also include at least one additional load, where at least a portion of the regenerative electrical energy is transmitted to the at least one additional load.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.