Patent · US Expired

Gas turbine engine carburetor with flat retainer connecting primary and secondary swirlers

US7131273B2 · kind B2 · utility

7Cited by
2References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 17, 2004
Grant dateNov 7, 2006
Priority date
Expiry dateJul 6, 2025

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23R2900/00018
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A gas turbine engine combustor carburetor includes forward and aft air swirlers. The aft swirler has a septum defining a primary venturi and a plurality of circumferentially spaced aft swirl vanes. The forward swirler has a plurality of circumferentially spaced forward swirl vanes extending forwardly from a flat annular radial flange of the forward swirler, an annular wall extending forwardly from a forward face of the septum and radially bounding an annular recess on the forward face, and the radial flange slidably retained within the annular recess and against the septum by a flat retainer attached to the annular wall of the septum. The flat retainer may be produced by stamping. An anti-rotation tab on the radial flange of the forward swirler extends radially through a corresponding notch in the annular wall.

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