Patent · US Active

Fuel control method for starting a gas turbine engine

US8915088B2 · kind B2 · utility

1Cited by
14References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 11, 2010
Grant dateDec 23, 2014
Priority date
Expiry dateMay 22, 2033

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2270/304
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method for controlling a flow of fuel to a starting gas turbine engine includes controlling the flow of fuel to the engine by controlling fuel pressure to the engine, and modulating the flow of fuel to the engine if engine exhaust gas temperature approaches a given exhaust gas temperature to lower the engine exhaust gas temperature below the given exhaust gas temperature.

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