Patent · US Active

Engine power supply circuit, and flight control member provided with such a circuit

US8669733B2 · kind B2 · utility

1Cited by
1References
4Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 30, 2010
Grant dateMar 11, 2014
Priority date
Expiry dateMar 30, 2030

Classification

  • Technology area (CPC H)Electricity
  • CPC primaryH02M7/5388
  • WIPO fieldElectrical machinery, apparatus, energy
  • WIPO sectorElectrical engineering

Abstract

A power supply circuit for an electric motor, the circuit comprising a plurality of inverter bridge arms, each having means for connection to a respective winding of the motor, each inverter bridge arm comprising in series a first insulated gate bipolar transistor and a junction field effect transistor that are connected to a controller, the circuit including a second insulated gate bipolar transistor connected in series with each field effect transistor and connected to the controller, and a damping resistor connected in parallel with the second bipolar transistor. An aircraft flight control member including a movable airfoil associated with at least one drive motor connected to such a power supply circuit.

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