Cooling unit cooling swirler vane of combustion burner

Patent metadata

Field	Value
Publication number	US-9593852-B2
Application number	US-201414340245-A
Country	US
Kind code	B2
Filing date	Jul 24, 2014
Priority date	Nov 29, 2007
Publication date	Mar 14, 2017
Grant date	Mar 14, 2017

Abstract

A combustion burner including a fuel nozzle, a burner tube that surrounds the fuel nozzle to form an air passage between the burner tube and the fuel nozzle, swirler vanes that are arranged in a plurality of positions in a circumferential direction on an external circumferential surface of the fuel nozzle, each of which extends along an axial direction of the fuel nozzle, and gradually curves from upstream to downstream, a liquid fuel injecting hole that is formed on the fuel nozzle, and from which a liquid fuel is injected to a vane pressure surface of each of the swirler vanes, and a cooling unit that cools a part of the vane pressure surface on which the liquid fuel hits. The cooling unit injects a mixed fuel prepared by mixing water and the liquid fuel evenly from the liquid fuel injecting hole to the vane pressure surface of the swirler vane.

First claim

The invention claimed is:

1. A combustion burner comprising:
a fuel nozzle;
a burner tube that surrounds the fuel nozzle to form an air passage between the burner tube and the fuel nozzle;
a plurality of swirler vanes being arranged in a plurality of positions in a circumferential direction on an external circumferential surface of the fuel nozzle, each of which extends along an axial direction of the fuel nozzle, and gradually curves from upstream to downstream so as to swirl air flowing in the air passage from the upstream to the downstream;
a liquid fuel injecting hole that is formed on the fuel nozzle and is configured to inject a liquid fuel to a vane pressure surface of each of the plurality of swirler vanes;
a static mixer disposed in the fuel nozzle and configured to mix water and the liquid fuel evenly to prepare a mixed fuel; and
a cooling unit that is configured to cool a part of the vane pressure surface on which the liquid fuel hits;
wherein the cooling unit injects the mixed fuel from the liquid fuel injecting hole to the vane pressure surface of each of the plurality of swirler vanes.

Assignees

• Mitsubishi Heavy Ind Ltd
• Mitsubishi Hitachi Power Sys

Inventors

• Saito Toshihiko
• Ishizaka Koichi
• Tanimura Satoshi

Classifications

• F23R3/14

  by using swirl vanes · CPC title

• F02C3/305

  Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids (F01K21/04 takes precedence) · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F02C3/30

  Adding water, steam or other fluids {for influencing combustion, e.g. to obtain cleaner exhaust gases (F02C7/141, F02C7/30, F01D21/00, F01K21/04, F23D11/10 take precedence)} · CPC title

• F23R2900/00004

  Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits · CPC title