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Multi-head double-fuel combined nozzle

A dual-fuel, multi-head technology, used in burners, injection devices, liquid injection devices, etc., can solve the problems of poor nozzle atomization, inconvenient installation and maintenance, and low combustion efficiency, and improve the quality of the outlet temperature field. , Easy installation and maintenance, and the effect of improving combustion efficiency

Inactive Publication Date: 2010-02-17
SHENYANG ENGINE DESIGN RES INST CHINA AVIATION IND CORP I
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problems of poor nozzle atomization effect, low combustion efficiency, complex structure and inconvenient installation and maintenance when using multiple dual-fuel nozzles to work in the current gas turbine combustor. , especially providing a multi-head dual-fuel combined nozzle

Method used

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  • Multi-head double-fuel combined nozzle

Examples

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Effect test

Embodiment 1

[0023] A multi-head dual-fuel combined nozzle. The multi-head dual-fuel combined nozzle in this embodiment includes a head nozzle 1, a central nozzle group 2, a nozzle mounting edge 3, a central liquid fuel nozzle mounting edge 4, and a nozzle housing 5; the nozzle housing 5 includes a head nozzle housing 6 and a central nozzle housing 7; the central nozzle group 2 includes a gas fuel nozzle 8, a duty nozzle 9, and a central liquid fuel nozzle 10; wherein the central liquid fuel nozzle 10 is a double Oil circuit centrifugal atomizing nozzle, the central liquid fuel nozzle 10 is connected with the central nozzle housing 7 through the central liquid fuel nozzle mounting edge 4; the central nozzle housing 7 passes through the center of the central nozzle group 2, and is formed by the right The side end surface protrudes; the head nozzle 1 is an independent dual-fuel nozzle, including three fuel passages of the first fuel passage 11, the second fuel passage 12, and the third fuel p...

Embodiment 2

[0028] A multi-head dual-fuel combined nozzle. The multi-head dual-fuel combined nozzle in this embodiment includes a head nozzle 1, a central nozzle group 2, a nozzle mounting edge 3, a central liquid fuel nozzle mounting edge 4, and a nozzle housing 5; the nozzle housing 5 includes a head nozzle housing 6 and a central nozzle housing 7; the central nozzle group 2 includes a gas fuel nozzle 8, a duty nozzle 9, and a central liquid fuel nozzle 10; wherein the central liquid fuel nozzle 10 is a double Oil circuit centrifugal atomizing nozzle, the central liquid fuel nozzle 10 is connected with the central nozzle housing 7 through the central liquid fuel nozzle mounting edge 4; the central nozzle housing 7 passes through the center of the central nozzle group 2, and is formed by the right The side end surface protrudes; the head nozzle 1 is an independent dual-fuel nozzle, including three fuel passages of the first fuel passage 11, the second fuel passage 12, and the third fuel p...

Embodiment 3

[0033] A multi-head dual-fuel combined nozzle. The multi-head dual-fuel combined nozzle in this embodiment includes a head nozzle 1, a central nozzle group 2, a nozzle mounting edge 3, a central liquid fuel nozzle mounting edge 4, and a nozzle housing 5; the nozzle housing 5 includes a head nozzle housing 6 and a central nozzle housing 7; the central nozzle group 2 includes a gas fuel nozzle 8, a duty nozzle 9, and a central liquid fuel nozzle 10; wherein the central liquid fuel nozzle 10 is a double Oil circuit centrifugal atomizing nozzle, the central liquid fuel nozzle 10 is connected with the central nozzle housing 7 through the central liquid fuel nozzle mounting edge 4; the central nozzle housing 7 passes through the center of the central nozzle group 2, and is formed by the right The side end surface protrudes; the head nozzle 1 is an independent dual-fuel nozzle, including three fuel passages: the first fuel passage 11, the second fuel passage 12, and the third fuel pas...

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Abstract

The invention relates to a multi-head dual fuel combined nozzle. The multi-head dual fuel combined nozzle is characterized by comprising a head nozzle 1, a center nozzle group 2, a nozzle mounting side 3, a center liquid fuel nozzle mounting side 4 and a nozzle casing body 5; the nozzle casing body 5 comprises a head nozzle casing body 6 and a center nozzle casing body 7; the center nozzle group 2comprises a gas fuel nozzle, a pilot nozzle 9 and a center liquid fuel nozzle10; the multi-head dual fuel combined nozzle has the advantages that the traditional mechanical structure is improved, thecombustion efficiency of the combustion chamber is enhanced, and the annihilation performance of the combustion chamber is improved. The multi-head dual fuel combined nozzle can be applied to the combustion turbine combustion chambers which are operated by adopting liquid fuel and gas fuel.

Description

technical field [0001] The invention relates to the mechanical field, and in particular provides a multi-head dual-fuel combined nozzle. Background technique [0002] When the gas turbine combustor uses gas fuel, such as natural gas, coke oven gas, etc., it generally needs to use liquid fuel, such as diesel, as a backup fuel to ensure that the gas turbine can still work normally when the gas fuel is lacking or suddenly interrupted, and the utilization rate of the gas turbine can be improved. Therefore, the nozzles installed on the gas turbine combustors are generally dual-fuel nozzles that can use both gaseous fuel and liquid fuel. At present, the installation of the nozzle and the flame tube of the gas turbine combustor mainly has the following two structural forms. The first structural form is that one flame tube corresponds to one dual-fuel nozzle, and the second structural form is that one flame tube corresponds to multiple dual-fuel nozzles. The nozzles are connected t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F23D17/00B05B7/00
Inventor 金戈顾铭企李孝堂尹家录
Owner SHENYANG ENGINE DESIGN RES INST CHINA AVIATION IND CORP I
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