Patent · US Expired

Fuel injector and multi-swirler carburetor assembly

US5930999A · kind A · utility

30Cited by
10References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 23, 1997
Grant dateAug 3, 1999
Priority date
Expiry dateJul 23, 2017

Classification

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

Abstract

A gas turbine engine carburetor includes a fuel injector having a plurality of circumferentially spaced apart fuel outlets. A plurality of air swirlers (24) are circumferentially spaced apart around the fuel injector (22), with each swirler having a fuel inlet (24b) disposed in flow communication with a respective one of the fuel outlets for receiving fuel therefrom. Each swirler includes a plurality of swirl vanes to swirl air for mixing with the fuel from the fuel inlets. The multi-swirler carburetor having a common fuel injector increases injection points for reducing NO.sub.x emissions.

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