Patent · US Active

Aircraft comprising an electric power distribution network

US12054280B2 · kind B2 · utility

0Cited by
0References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 21, 2022
Grant dateAug 6, 2024
Priority date
Expiry dateFeb 3, 2043

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D2221/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft including a first electrical distribution busbar and a second electrical distribution busbar extending at least in part in a fuselage of the aircraft, in a longitudinal direction of the fuselage. A first electric generator is connected to the distribution conductors of the first electrical distribution busbar via a first coupling switch directly connected to the first electric generator and to the distribution conductors of the first busbar. A second electric generator is connected to the distribution conductors of the second electrical distribution busbar via a second coupling switch directly connected to the second electric generator and to the distribution conductors of the second busbar. The first coupling switch and the second coupling switch are positioned in the aircraft independently of one another.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.