Patent · US Active

Fuel injector

US8733105B2 · kind B2 · utility

6Cited by
9References
17Claims
0Family size

Assignee

Inventor

Key dates

Filing dateOct 5, 2009
Grant dateMay 27, 2014
Priority date
Expiry dateNov 22, 2032

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF23D2900/11101
  • WIPO fieldThermal processes and apparatus
  • WIPO sectorMechanical engineering

Abstract

A fuel injector for a fuel spray nozzle of a gas turbine engine combustor is provided. The fuel injector has an annular flow passage which conveys fuel to a prefilming lip at an end of the flow passage. The fuel injector also has plurality of fuel distributor slots which are circumferentially spaced around and in fluid communication with the other end of the flow passage to deliver respective fuel streams into the flow passage. The slots are configured so that the fuel streams enter the flow passage at a swirl angle of at least 80° relative to the axis of the flow passage.

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