EP1512912A3

Homogeneous mixture formation by swirled injection of the fuel

Abstract

The invention relates to a fuel injection device for a gas turbine, with a flow channel 1 for an air flow, at the flow walls 2 at least one fuel port 3 is formed for introducing fuel into the air flow, wherein the central axes 4 of the fuel ports 3 are arranged inclined at least in the circumferential direction ,

EP1512912A3, drawing sheet 1
Sheet 1 of 2

Term

Term ended

Projected expiry passed 27 August 2024, 2.1 years ago.

  1. Priority
  2. Filed
  3. Published
  4. Projected expiry
  5. Today

2 sheets

  1. Sheet 1
  2. Sheet 2