Nova Patents
EP1526332A3

Fuel injection nozzle

Abstract

The invention relates to a fuel injection nozzle for a gas turbine combustor, with a film former 1, in which a plurality of fuel openings 2 are formed. The invention is characterized in that the central axes 5 of the fuel openings 2 are arranged by the film feeder 1 with respect to their radial orientation substantially parallel to the main flow direction 6 of the air.

EP1526332A3, drawing sheet 1
Sheet 1 of 1

Term

Term ended

Projected expiry passed 6 October 2024, 2 years ago.

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

1 sheet

  1. Sheet 1