Patent · US Active

Multi-rotor aircraft propulsion system with reconfigurable electric network

US11827374B2 · kind B2 · utility

0Cited by
1References
9Claims
0Family size

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Key dates

Filing dateMar 25, 2019
Grant dateNov 28, 2023
Priority date
Expiry dateOct 8, 2040

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

In the field of multi-rotor rotary-wing aircraft a propulsion system for such an aircraft includes a reconfigurable electric network for supplying the electric motors driving the rotors. The system includes: a supply source, a supply bus connected to the supply source, at least four drive units each including an electric motor and its control circuit, and an electrical ring network including: an electrical line which is interrupted at each drive unit and whose ends are connected to the supply bus, and, for each drive unit, a first switch and a second switch that are connected between the control circuit and the electrical line, on either side of the interruption.

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