Patent · US Active

Aircraft taxiing system

US9815550B2 · kind B2 · utility

0Cited by
3References
13Claims
0Family size

Assignees

Inventors

Key dates

Filing dateSep 25, 2015
Grant dateNov 14, 2017
Priority date
Expiry dateMay 19, 2036

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/80
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A taxiing system for an aircraft including an undercarriage having a wheel, includes an electric motor associated with the wheel, an electric controller of the electric motor, connected to an output of an electrical power supply, and a taxiing control computer configured to determine control instructions for the electric motor and to transmit these instructions to the electric controller. The taxiing control computer is configured to receive braking of the aircraft commands during the taxiing of the aircraft and to determine control instructions for the electric motor corresponding to operation of the motor in generator mode when it receives a braking command. The electric controller is connected to an energy absorber making it possible to absorb the electric energy produced by the electric motor when the latter is operating in generator mode.

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