Patent · US Active

Method and system for taxiing an aircraft

US7802757B2 · kind B2 · utility

42Cited by
14References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 9, 2005
Grant dateSep 28, 2010
Priority date
Expiry dateSep 4, 2028

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2220/76
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The system is used for taxiing an aircraft and comprises at least one multi-spool gas turbine engine, the engine having an electrical motor in a torque-driving engagement with a low pressure spool of the engine. The low pressure spool has a propulsor connected thereon to generate thrust when rotated. A controller is connected to the electrical motor and an electrical power source to control an amount of electrical power provided from the power source to the electrical motor so as to drive the propulsor and cause at least a major portion of the thrust to be generated by the propulsor for moving the aircraft during taxiing.

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