| 摘要 |
The disclosure concerns a nozzle (1) for a gas turbine combustor, the nozzle (1) comprising an inner channel (3), a swirl channel (4), a mixing zone (5) and an outlet channel (6), wherein the nozzle (1) extends from an inlet (20) to an outlet (22), the swirl channel (4) is disposed around the inner channel (3), the inner channel (3) and the swirl channel (4) extend from the inlet (20) to the mixing zone (5), the mixing zone (5) extends from the inner channel (3) and the swirl channel (4) to the outlet channel (6), and the outlet channel (6) extends from the mixing zone (5) to the outlet (22). A burner (8) and a gas turbine comprising the nozzle (1) are also described, along with a method of using the nozzle (1). |
