Patent · US Active

Modular fuel nozzle air swirler

US7658339B2 · kind B2 · utility

10Cited by
8References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 20, 2007
Grant dateFeb 9, 2010
Priority date
Expiry dateFeb 7, 2028

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R3/283
  • WIPO fieldChemical engineering
  • WIPO sectorChemistry

Abstract

A modular fuel nozzle air swirler for a gas turbine engine has a body defining a fuel passage extending between an inlet end and a discharge end of the body. An annular cap is removably secured to the discharge end of the body via cooperating interlocking members.

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