Patent · US Expired

Flamesheet combustor

US6935116B2 · kind B2 · utility

42Cited by
24References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 28, 2003
Grant dateAug 30, 2005
Priority date
Expiry dateMay 29, 2023

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R3/286
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine combustion system having reduced emissions and improved flame stability at multiple load conditions is disclosed. The improved combustion system accomplishes this through complete premixing, a plurality of fuel injector locations, combustor geometry, and precise three dimensional staging between fuel injectors. Axial, radial, and circumferential fuel staging is utilized including fuel injection proximate air swirlers. Furthermore, strong recirculation zones are established proximate the introduction of fuel and air premixture from different stages to the combustion zone. The combination of the strong recirculation zones, efficient premixing, and staged fuel flow thereby provide the opportunity to produce low emissions combustion at various load conditions.

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