Patent · US Active

Hybrid aircraft having rectifier with integrated protection

US11840148B2 · kind B2 · utility

1Cited by
2References
14Claims
0Family size

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Inventors

Key dates

Filing dateFeb 15, 2022
Grant dateDec 12, 2023
Priority date
Expiry dateFeb 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.