Cooling unit for swilrer vane of combustion burner

Patent metadata

Field	Value
Publication number	US-9574775-B2
Application number	US-201414340210-A
Country	US
Kind code	B2
Filing date	Jul 24, 2014
Priority date	Nov 29, 2007
Publication date	Feb 21, 2017
Grant date	Feb 21, 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 circumferential direction on an external circumferential surface of the fuel nozzle, 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 includes a multi-purpose injecting hole that is arranged on the vane pressure surface of each of the swirler vanes, and from which a gas fuel is injected during gas combustion, and water is injected to the vane pressure surface of the swirler vane during combustion of the liquid fuel.

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 from which a liquid fuel is injected to a vane pressure surface of each of the plurality of swirler vanes; and
a cooling unit that cools a part of the vane pressure surface on which the liquid fuel hits;
wherein the cooling unit includes multi-purpose injecting holes that are respectively arranged on the vane pressure surface of each of the plurality of swirler vanes, the multi-purpose injecting holes being configured to receive injected gas fuel during gas combustion, and being configured to receive water injected to the vane pressure surface of the plurality of swirler vanes during combustion of the liquid fuel.

Assignees

• Mitsubishi Heavy Ind Ltd
• Mitsubishi Hitachi Power Sys

Inventors

• Saito Toshihiko
• Ishizaka Koichi
• Tanimura Satoshi

Classifications

• F23R3/283 Primary

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title

• F02C7/22

  Fuel supply systems · CPC title

• F23R3/38

  comprising rotary fuel injection means · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F23R3/14

  by using swirl vanes · CPC title