Patent · US Active

System for detecting ignition failure in a gas turbine engine

US7664590B2 · kind B2 · utility

4Cited by
4References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 29, 2008
Grant dateFeb 16, 2010
Priority date
Expiry dateOct 17, 2028

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02C9/36
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A method of operating a gas turbine engine is provided. The method includes introducing a fuel into a combustor, detecting a failure of ignition of the fuel, and preventing ignition until the introduced fuel is substantially removed from the gas turbine engine.

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