Patent · US Active

Gas turbine fuel control system

US10145309B2 · kind B2 · utility

0Cited by
24References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 5, 2015
Grant dateDec 4, 2018
Priority date
Expiry dateJul 21, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/31
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method of controlling a flow of a fuel mixture of different types of fuel in a gas turbine engine is described which includes determining a combustive energy value of an input of the fuel mixture in the engine, extracting fuel schedule data from a fuel schedule established for a reference fuel, determining a desired fuel mixture flow rate by adapting the fuel schedule data to the fuel mixture based on the combustive energy value, and controlling a fuel metering device of the engine such that the fuel mixture flow rate corresponds to the desired fuel mixture flow rate.

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