Patent · US Active

Apparatus and method for reducing aircraft fuel consumption

US8290683B2 · kind B2 · utility

14Cited by
47References
28Claims
0Family size

Assignee

Inventor

Key dates

Filing dateFeb 16, 2010
Grant dateOct 16, 2012
Priority date
Expiry dateJan 18, 2031

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/07
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method and apparatus for improving fuel efficiency in an aircraft having a digital avionics system and at least first and second engines. The avionics system includes first and second full-authority digital engine control (FADEC) systems and corresponding first and second engines. At least one processor is provided that is programmed with a differential specific fuel consumption (DSFC) algorithm and first and second engine optimization algorithms. The DSFC algorithm adjusts the throttle of the first and second engines to substantially equalize the differential specific fuel consumption of the engines and thereby improve the fuel efficiency of the aircraft. The first and second engine optimization algorithms adjust at least one operating parameter of the first and second engines respectively to improve the fuel efficiency of the first and second engines.

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